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Garmin Software Version 0508.10 Cockpit Reference Guide

1. 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 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Press the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Press the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 5 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 39 ACN Sd5 S24V oipny uadx sia su uini sul sub buluueld Wil e uepioAy s mp old paezey s m ie q jeuonippy s y uone1ado junuuy Jeuuouqy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN 40 Displaying Traffic on the Navigation Map 1 Ensure TIS is operating With the Navigation Map displayed press the MAP Softkey 2 Press the TRAFFIC Softkey Traffic is
2. PFD1 DB ERR PFD1 terrain database error exists The MFD and or PFD detected a failure in the errain database Ensure that the terrain card s properly inserted in display Replace terrain card If problem persists the G1000 system should be serviced MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced 60 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN Annunciations 8 Alerts DATABASE MESSAGE ADVISORIES CONT Message Comments MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing The obstacle database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing The MFD and or PFD detected a failure in the a
3. GMAT FAIL GMAT is inoperative The audio panel self test has detected a failure The audio panel is unavailable The G1000 system should be serviced GMA XTALK GMA crosstalk error has occurred An error has occurred in transferring data between the two GMAs The G1000 system should be serviced GMA1 CONFIG GMAT config error Config service req d The audio panel configuration settings do not match backup configuration memory The G1000 system should be serviced MANIFEST GMA1 software mismatch communication halted The audio panel has incorrect software installed The G1000 system should be serviced GMA1 SERVICE GMA1 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 G1000 system should be serviced when possible 62 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN GIA 63 MESSAGE ADVISORIES Annunciations amp Alerts Message Comments f Con GIA1 CONFIG GIA1 config error ig service req d f Con GIA2 CONFIG GIA2 config error ig service req d The GIA1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced GIA1 CONFIG GIA1 aud error Config service req d GIA2 CONFIG
4. 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 658 16 A GARMIN GPS Navigation GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation from the MFD 1 Press the Direct to 9 Key 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 sia s u uinnsu oipny uadx U10 AEN sub 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 41 a Duruue d nf proceed to step 9 8 Tum the small FMS Knob to select MSL or AGE 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field 10 Enter the desired offset distance before the waypoint 11 Press the ENT Key The Activate field is highlighted 12 Press the ENT Key to activate Direct to Navigation from the PFD 1 Press the Direct to Key E 2 Tum the large FMS Knob to place the cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTI
5. Press the FPL Key on the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Press the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 1 2 3 4 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint Press the ACT LEG Softkey on the MFD OR Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B GARMIN Ps Navigation STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This does not delete the stored flight plan only the active flight plan VERTICAL NAVIGATION The navigation database only contains alti
6. UTE Blank Page 6 2 4 eouepioAy paezey s m Jeuonippy uoneiedo Jeuuouqy sue v unuuy xipuaddy x pul 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 658 30 A GARMIN Procedures PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Tum the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure is active when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key on the MFD to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired waypoint within the departure 4 Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Tum
7. 48 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN Additional Features 4 Turn the small FMS Knob to choose between the On and Off Full Screen Options 5 Tum the small FMS Knob to choose between Day Auto and Night Options 6 In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity 7 Press the FMS Knob when finished to remove the Chart Setup Menu XM RADIO ENTERTAINMENT The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select the displayed AUX XM Information Page 3 Press the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio 1 Press the CATGRY Softkey on the XM Radio Page 2 Press the CAT and CAT Softkeys to cycle through the categories O
8. NOTE Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset 190 00526 01 Rev B System Information Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 35 35 ww A k IN HG 10 10 21 2 21 5 re 57 2320 2320 SYSTEMN Lo cu m 52 b 58 41 0 PSI 40 0 FUEL CALC GAL REM 161 3 GAL USED 4 7 ELECTRICAL i mgr R 40 LOAD Z 34 E BUS R 28 5 VOLTS 27 4 SYSTEM Engine Page Fuel Calculation Information Electrical Information sjueumansu say uone1ado SoJnjeaJ aueploay sainparold buluueld AEN Sd5 241V oipny uadx unuuy Jeuuouqy Jeuonippy UI10 AEN xipuaddy xepu UTE 2 GARMIN Engine Indication System s u uin sul fila oipnv uadx 010 AEN S2dV AeN Sd5 Buruuejd Blank Page 6 2 4 eouepioAy paezey sainjea4 jeuonippy uoneiedo Jeuuouqy sue v unuuy xipuaddy x pul 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 658 A GARMIN NAV COM TRANSPONDER AUDIO PANEL ADF TUNING OPTIONAL Tune the ADF using the remote ADF control head DME TUNING OPTIONAL 1 Press the DME Softkey 2 Tum the large FMS to select the DME source field 3 Turn the small FMS Knob to select the desired DME tuning 4 Press the ENT Key to complete the selecti
9. Sue v uoneiedo SoJnjeaJ junuuy jeuuouqy jeuonippy xipuaddy Flight Instruments Nav Com GPS Nav XPDR Audio EIS Flight Planning Hazard Avoidance Procedures Annun Abnormal Additional Alerts Operation Features Appendix Index A Hazard Avoidance GARMIN 38 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 Echo Top Cloud Top and Echo Top Mutually Exclusive Cell Movement City Forecast Freezing Levels Cyclone Warnings MEIARS Surface Analysis County Warnings Cloud Top SIGMETs AIRMETs Winds Aloft Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B GARMIN Hazard avoidance TRAFFIC SYSTEMS If Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE softkeys are displayed Ifa Traffic Advisory System TAS is configured STANDBY OPERATE TEST and ALT MODE softkeys are displayed Traffic Symbol Description e Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory TA closing rate distance and vertical separation meet TA criteria Q Traffic Advisory Off Scale Traffic Symbol Description Traffic Information Service TIS
10. 6 7 Press the FPL Key Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint after the desired airway entry point If this waypoint is not a valid airway entry point a valid entry point should be entered at this time Turn the small FMS Knob one click clockwise and select the LD AIRWY Softkey or press the MENU Key and select Load Airway The Select Airway Page is displayed The LD AIRWY Softkey or the Load Airway menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown first in the list followed by all altitude airways and then high altitude airways Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted Press the ENT Key The system returns to editing the flight plan with the new airway inserted INVERT AN ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the MENU Key to display the Page Menu Turn the large FMS Knob to highlight Invert Flight Plan Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location With OK highlighted press the ENT Key to invert the flight plan REMOV
11. 9 FLIGHT PLANNING 21 Trip Planning te t te o t n e o c E RE 21 Create a New User Waypoint sssssssse nn 22 Delete a User 1 4 23 Create a New Flight Plan 24 i 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 658 A Table of Contents GARMIN Insert a Waypoint in the Active Flight Plan sse 25 Enter an Airway in a Flight Plan Invert An Active Flight Plan Remove a Departure Arrival Approach or Airway from a Flight Plan 26 Store a Flight Plan eoe rere ie leti 2 Edit a Stored Flight Plan 2 Delete a Waypoint from the Flight Plan sss 2 Invert and Activate a Stored Flight 6 28 Copy a Flight Pl n eee eet b n ern Delete a Flight Plan Graphical Flight Plan Creation PROCEDURES a Ad tert piece ette Uu Load and Activate a Departure Procedure Activate A Departure Leg Load An Arrival Procedure seen Activate An Arrival Leg sss Load and or Acti
12. G1000 system should be serviced T MANIFEST GWX software mismatch The GWX 68 has incorrect software installed T GWX 68 ALERT MESSAGES CONT Message Comments WX ALERT Possible severe weather ahead of 80 to 320 nm The GWX 68 indicates severe weather within 10 degrees of the aircraft heading at a range MISCELLANEOUS MESSAGE ADVISORIES Message Comments FPL WPT LOCK Flight plan waypoint is locked Upon power up the G1000 system detects that a stored flight plan waypoint is locked This occurs when an aviation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message also occur with user waypoints in a flight p is deleted Remove the waypoint from the flight plan i f This can an that 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 aviation database update Verify that stored flight plans contain correct waypoint locations 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 S9Jnjeo4 e uepioAvy s mp old buluueld ACN 540 52 404 sia s u u nnsul paezey wy wio gt Aen 10614 uoneiedQ jeuuouqy x2 5 x pul Fligh
13. Presets Up to 15 channels from any category can be assigned a preset number 1 2 3 4 On the XM Radio Page with the desired channel active press the PRESETS Softkey to access the first five preset channels PS1 PS5 Press the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Pressing the MORE Softkey repeatedly cycles through the preset channels Press any one of the PS1 PS15 softkeys to assign a number to the active channel Press the SET Softkey on the desired channel number to save the channel as a preset Adjusting Volume 1 2 3 4 On the XM Radio Page press the RADIO Softkey Press the VOL Softkey to access the volume control softkeys Press VOL or VOL softkeys to adjust the volume level Press the MUTE Softkey to mute the radio audio Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B GARMIN operation ABNORMAL OPERATION REVERSIONARY MODE Should a system detected failure occur in either display the G1000 automatically enters reversionary mode In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display Minimal navigation capability is available on the reversionary mode display Reversionary display mode can be manually activated by pressing the DISPLAY BACKUP Button on the audio panel NOTE The Beechcraft
14. Press 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 MFD to display the Active Flight Plan Page Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion point Press the LD WPT Softkey The selected waypoint is inserted at the selected point The default user waypoint naming is USR000 USR001 USR002 and so on To change the user waypoint name follow the procedure for modifying a user waypoint 29 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 oipny dadx 53 Sjuouinajsu U10 AEN aui S24V s mp old Buruuejd AEN Sd5 nubi Sue v uonejedo sainqea4 e uepioAy unuuy jeuuouqy jeuonippy paezey xipuaddy x pul GARMIN Flight Planning s u uin sul fil 59 olpny dddX 010 AEN S2dV AeN Sd5 Duruue d
15. RAIM is not lt ailable from FAF to MAP waypoints GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity Monitoring RAIM from the FAF to the MAP waypoints with other NAVS LOI GPS integrity lost Crosscheck Loss of GPS integrity monitoring GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure Abort approach ABORT APR Loss of GPS navigation Abort approach due to loss of GPS navigation Change hdg reference to TRUE TRUE APR True north approach Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO 64 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN Annunciations 8 Alerts GIA 63 MESSAGE ADVISORIES CONT Message Comments GPS1 FAIL GPS1 is inoperative GPS2 FAIL GPS2 is inoperative A failure has been detected in the GPS1 and or GPS2 receiver The receiver is unavailable The G1000 system should be serviced GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service A failu
16. a sustained slip skid indicator is centered maximum fuel imbalance lim its force Ensure the and observe any A condition has developed causing the yaw Servo to provide a sustained slip skid indicator is centered maximum fuel imbalance lim Performing preflight system t completion the aural alert w force Ensure the and observe any its est Upon ill be heard Preflight system test has failed 57 Garmin 61000 Cockpit Reference Guide for the Beechcraft 58 G58 s m ie q UED OAV s mp old buluueld ACN 540 92 404 sia Sjueuinajsu paezey wy wio gt Aen 10614 jeuonippy uoneiedQ jeuuouqy x2 5 x pul A Annunciations amp Alerts GARMIN TAWS SYSTEM STATUS ANNUNCIATIONS Flight Instruments Alert Type Hm MY Fage Aural Message Annunciation TAWS System Test Fail TAWS FAIL TAWS System Failure TAWS Alerting is disabled TAWS INHB No GPS position or excessively TAWS N A TANS Not Available Nav Com XPDR Audio degraded GPS signal TAWS Available will be heard when sufficient GPS Signal is re established System Test in progress TAHS TEST System Test pass None TANS System Test OK VOICE ALERTS AFCS GPS Nav Flight Planning Voice Alert Description Minimums minimums f The aircraft has descended below the preset barometric minimum descent altitude 1 V f he aircraft
17. detected a problem The G1000 system should be serviced MANIFEST PFD1 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The G1000 system should be serviced PFD1 CONFIG PFD1 config error Config service req d The PFD configuration settings do not match backup configuration memory The G1000 system should be serviced MFD1 CONFIG MFD1 config error Config service req d The MFD configuration settings do not match backup configuration memory The G1000 system should be serviced SW MISMATCH GDU software version mismatch Xtalk is off The MFD and PFD have different software versions installed The G1000 system should be serviced PFD1 COOLING PFD1 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the G1000 system should be serviced PFD1 KEYSTK PFD1 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists 190 00526 01 Rev B 59 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 s
18. music Copilot passengers music Copilot Selected radios pilot copilot Selected radios pilot copilot passengers music Copilot passengers music Selected radios pilot passengers music Passengers music Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 Nav Com XPDR Audio Panel sjueumansu 52 oipny uddx 93 UI0JNeN Sue v uonejedo So1nje2J e uepioAy SoJnpa20Jd Buiuue d AEN 5640 junuuy jeuuouqy jeuonippy xipuaddy x pul UTE 2 GARMIN Nav Com XPDR Audio Panel Blank Page 6 2 4 x pul 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 658 12 A GARMIN AUTOMATIC FLIGHT CONTROL SYSTEM 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 AFCS NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in the following table when the flight director is not active activates the pilot side flight director in the listed modes Modes Selected Control Pressed Lateral Vertical FD Key Roll Hold default ROL Pitch
19. 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 Displaying Weather on the Weather Radar Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Weather Radar Page Press the MODE Softkey If the aircraft is on the ground press the STANDBY Softkey to initiate the one minute warm up period After the warm up is complete the radar 43 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 AEN Sd9 52 oipny dadx Si Sjuouinajsu u102 AEN 3461 nf e uepioAy s mp old paezey Sue v uoneiedo SoJnjeaJ junuuy jeuuouqy jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN enters Standby Mode After the aircraft is airborne press the WEATHER Softkey Or If the aircraft is already airborne press the WEATHER or GROUND Softkey The one minute warm up period is initiated after which the radar begins transmitting The horizontal scan is initially displayed 5 Turn the Joystick to select the desired range 6 If desired press the VERTICAL Softkey for vertical scanning Adjusting Antenna Tilt Move the Joysti
20. using other navigation equipment until GPS derived position data is restored 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 3 SoJnpa20Jd Buiuue d AEN 540 2 olpny uqax 913 sjueumansu wio gt AeN paezey SoJnjeo4 Sue v unuuy xipuaddy x pul 3461 Wila Nav Com XPDR Audio Hazard Additional Flight Instruments Flight Planning EIS AFCS GPS Nav Avoidance Procedures Features Annun Alerts Appendix Index Abnormal Operation 54 A GARMIN SUM Paes CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following Navigation Status Box fields except Active Leg TAS and DIK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD Track Bug All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will not couple to GPS and both TAWS and Terrain Proximity are disabled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but w
21. 58 G58 Pilot s Operating Handbook POH always takes precedence over the information found in this section ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected In the event of a failure of both PFDs the emergency frequency 121 500 MHz automatically becomes the active frequency on both COM radios HAZARD DISPLAYS WITH LOSS OF GPS POSITION If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are removed until GPS position is again established HULULULU Loss of Hazard Functions vvith Loss of GPS Position 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 92uepioAy s mp old buluueld AEN Sd5 241V orpny dadx sia Sjueuinajsu 2 s m ie q Sue v unuuy xipuaddy x pul sub Wfl paezey Flight Instruments Nav Com XPDR Audio Flight Planning Additional Hazard Avoidance Annun EIS AFCS Alerts Features Procedures GPS Nav Appendix Index Abnormal Operation UNUSUAL ATTITUDES functions are displayed in these situations are disabled when the aircraft experiences unusual attitudes 52 Traffic Annunciations AFCS Annunciations Flight director Com mand Bars Inset Map Temperatur
22. APPENDIX sjuaumnasu Wil PFD SOFTKEY MAP 993 optional mer L 1 Loe Gee Deewr ST TS noes wv nnnnnun 7 oipny uadx U10 AEN CDI NAV2 S2dV Top Level PFD Softkeys 2 Vsser 1 EY r YU xY mu H US r optional optional optional Core boca L reser vero TERRAN ERs neeo e mack ALERTS 3 nnn n amp mnmmmamnmn a Press the BACK Softkey to return to the top level softkeys aoueplony paezey Inset Map Softkeys s m ie q jeuonippy INSET Displays Inset Map in PFD lower left corner 2 2 OFF Removes Inset Map DCLTR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan Sue v unuuy gt 5 o x pul 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 15 Annun Abnormal Additional Hazard Flight Nav Com Flight Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index A GARMIN Appendix TRAFFIC Displays traffic information on Inset Map TOPO Displays topographical data e g coast lines terrain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map STRMSCP Press to display the Storm
23. ARMIN Garmin nternational Inc Garmin Europe Ltd Liberty House Bulls Copse Roa Hounsdown Business Park Southampton SO40 9RB U K p 44 0870 8501241 f 44 0870 850125 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 www garmin com 2005 2007 2008 Garmin Ltd or its subsidiaries 190 00526 01 Rev B
24. Automatic Standby When the weather radar system is in the Weather or Ground Map Mode upon landing the system automatically switches to Standby Mode 46 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B GARMIN Additional Features ADDITIONAL FEATURES NOTE The availability of SafeTaxi ChartView or FliteCharts in electronic form does not preclude the requirement to carry paper charts aboard the aircraft See AC 120 76A for more information SAFETAXI SafeTaxi is an enhanced feature that gives greater map detail when zooming in on airports at close range The airport display on the map reveals runways with numbers taxiways with identifying letters numbers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges When the aircraft location is within the screen boundary including within SafeTaxi ranges an airplane symbol is shown on any of the navigation map views for enhanced position awareness 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 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 ba
25. E A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT 26 1 PLAN Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key on the MFD Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B GARMIN ight Planning b Turn the small FMS Knob to select the Flight Plan Catalog Page c Press the FMS Knob to activate the cursor d Turn the large FMS Knob to highlight the desired flight plan e Press the EDIT Softkey 2 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 sjuaumasu 346 s q oipny uadx U10 AEN 3 Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN S24V AEN Sd5 1 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key 2 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key 3 With OK highlighted press the ENT Key to store the flight plan v pu i8 sx 2 EDIT A STORED FLIGHT PLAN 1 Press the FPL Key on the MFD then turn the small FMS Knob to display the Flight Plan Catalog Page 2 Press the FMS Knob to activate the cursor 3 Tu
26. G1000 Integrated Flight Deck Cockpit Reference Guide for the Beechcraft 58 G58 GARMIN Copyright 2005 2007 2008 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0508 10 or later or 0857 00 WAAS or later for the Beechcraft 58 G58 Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton 5040 ORB U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 Web Site Address www garmin com Except as expressly provided herein no part of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be v
27. GARMIN 0 ble of Contents Hazard Displays with Loss of GPS Position sss 51 Unusual Attitudes ee eer gem tese dem dre 52 Dead Reckoning eee ierit e tite e io ie di 53 ANNUNCIATIONS amp ALERTS 55 WARNING Annunciation CAUTION Annunciation sse ADVISORY Annunciation Alert Message eee nette tite ine baie ne BULA AFCS ALERTS ERU ene TAWS System Status Annunciations Voice Alerts ceto trees 0 quan o deu MFD amp PFD Message Advisories sssssssseenne MFD amp PFD Message Advisories Cont Database Message Advisories GMA 1347 Message Advisories sssssssssseeene GIA 63 Message Advisories GIA 63W Message Advisories GEA 71 Message Advisories GTX 33 Message Advisories GRS 77 501165 GMU 44 Message Advisories GDL 69A Message Advisories seen GDC 74A Message Advisories ssssssseeeenne GWX 68 Alert Messages GWX 68 Alert Messages Cont Miscellaneous Message Advisories sssssss 71 APPENDIX sa 75 PFD Softkey cccccccccssssssssssssssssssssssssssssssssscsssssssssscesssssvsssscesssssssssseessssnssssecesansns
28. GIA2 aud error Config service req d io con io con p The GIA1 and or GIA2 have an error in the audio configuration The G1000 system should be serviced too low GIA1 COOLING GIA1 temperatu e too low GIA2 COOLING GIA2 temperatu The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature temperature GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be serviced GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The G A1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced MANIFEST GIA1 communication halted software mismatch MANIFEST GIA2 communication halted COM1 TEMP 1 over temp Reducing transm itter power software mismatch itter power COM2 TEMP COM2 over temp Reducing transm The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced 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 G1000 system should be serviced 190 00526 01 Rev B 63 Ga
29. Hold default PIT AP Key Roll Hold default ROL Pitch Hold default PIT CWS Switch Roll Hold default ROL Pitch Hold default PIT GA Switch Go Around in air GA Go Around in air GA ALT Key Roll Hold default ROL Altitude Hold ALT VS Key Roll Hold default ROL Vertical Speed VS 7 7 Roll Hold default ROL Vertical Path Tracking VPTH GPS NAV Key Navigation VOR Pitch Hold default PIT LOC GPS APR Key Approach VAPP Pitch Hold default PIT LOC HDG Key Heading Select HDG 1 Pitch Hold default PIT Valid VNV flight plan must be entered before VNV Key press activates flight director The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAVor APR Key press activates flight director 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 913 sjueumansu oipny uadx U10 AEN ACN Sd5 52 Sue v uonejedo So1nje2J e uepioAy SoJnpa20Jd Buiuue d junuuy jeuuouqy jeuonippy xipuaddy xepu UTE paezey A GARMIN Appendix Selected Altitude Index is to be captured instead of VNV Target Altitude ALTV armed automatically under VPTH when VNV Target Altitude is to be captured instead of Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 AFCS s VERTICAL MODES E Vertical Mode Description Control Annunciation Holds the current aircraft pitc
30. I Sue v uonejedo saunqea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS GPS Nav Procedures Appendix Alerts Operation Features Index Flight Instruments Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 A GARMIN 190 00526 01 Rev B A GARMIN Engine Indication System ENGINE INDICATION SYSTEM ENGINE DISPLAY In all cases green indicates normal operation yellow indicates caution and red indicates warning Pressing the ENGINE Softkey makes available the LEAN and SYSTEM softkeys which in turn provide access to the Lean Page and the System Page respectively Manifold Pressure Gauge Left Engine RPM Gauge Left Engine Fuel Flow Indicator Oil Temperature ndicator Ammeter 190 00526 01 Rev B A o k IN HG 10 10 27 2 276 Neate 2320 2320 FFLOW 10 6 GPH 89 HIR 0 30 OIL TEMP g 6 OIL PRES iL a ALT LOAD iL R FUEL QTY GAL Default Engine Page Propeller Sync indicator Fuel Flow Numeric Readout 27 Head emperature Indicator Oil Pressure Indicator Fuel Quantity Indicator Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 sjueumansu x 5 gt o sue v uonejedo So1nje2J aou
31. IN Selecting FPL 00 displays the active flight plan If an active flight plan is selected REM is an available option to display planning data for the remainder of the flight plan NOTE The page mode must be set to MANUAL to perform the following steps Turn the large FMS Knob to highlight the departure time DEP TIME field NOTE The departure time on the Trip Planning Page is used for preflight planning Refer to the Utility Page for the actual flight departure time Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system The flashing cursor moves to the fuel onboard field Modify the fuel onboard Press the ENT Key when finished The flashing cursor moves to the calibrated airspeed field Enter a calibrated airspeed Press the ENT Key when finished CREATE A NEW USER WAYPOINT 22 1 2 3 4 5 6 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Press 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 REFERENCE WAYPOINTS field If desired the waypoint can be defined by a reference waypoint
32. IVATE is now displayed with LOAD highlighted 8 Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and is immediately UJ AEN Sd5 24V oipny uadx s z sjueumasuj JU05 AEN 346 4 Juil activated 9 Press the ENT Key ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL 3 Press the ENT Key 4 The final approach course becomes the active leg 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 33 SeJnpa20Jd Sue v uonejedo saunqea4 e uepioAy junuuy jeuuouqy jeuonippy xipuaddy x pul puezey Nav Com XPDR Audio Procedures Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index A Procedures 027 GARMIN ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 34 1 2 3 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH Press t
33. N Softkey to return to the Horizontal Scan view and repeat the previous steps Adjusting Gain WARNING Changing the gain in Weather Mode causes precipitation intensity to be displayed as a color not representative of the true intensity Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation 1 Press the GAIN Softkey to activate the cursor in the GAIN field 2 Tum 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 Press the GAIN Softkey again to recalibrate the gain CALIBRATED is displayed in the GAIN field Ground Mapping 1 Press the MODE Softkey 2 Press the GROUND Softkey to place the radar in Ground Map Mode 3 Press the BACK Softkey 4 Press the FMS Knob to activate the cursor 5 Turn the large FMS Knob to place the cursor in the TILT field 6 Adjust the antenna tilt angle by turning the small FMS Knob to position the ground returns as desired 7 Press the FMS Knob to remove the cursor 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 becomes the center point of the Sector Scan 2 Press the FMS Knob to display
34. NE INDICATION SYSTEM 5 Engine Display eren etn eter aet 5 Lean Engine Display sssssseeeneennnn nennen 6 Engine System Display 7 NAV COM TRANSPONDER AUDIO 9 ADF Tuning s s s s s s s s s s s sis ss s s l 9 DME Tuning Optional 00 c cccsssssssssssssssssssssssssssssssssvssssscessssvsssscessssssessecesassnssssess 9 Enter a Transponder Code sees 9 Selecting a COM Radio seen 9 Selecting 0 NAV COM odda tht tt et rm ch ee 0 Digital Clearance Recorder and Player 0 Intercom System ICS Isolation 1 AUTOMATIC FLIGHT CONTROL 5 9 3 Flight Director Activation sss 3 Vertical Modes am ee ania teh ete id Rc 4 Lateral Modes 5 GPS NAVIGATION o aaa ad a 7 Direct to Navigation sssssssseeee nnne 7 Activate a Stored Flight Plan 8 Activate a Flight Plan Leg 8 Stop Navigating a Flight Plan 9 Vertical Navigation ssssssseeeenenennenntnnnnnnnnns
35. Return the unit for repair GIA2 SERVICE GIA2 needs service The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced HW MISMATCH GIA ha rdware mismatch GIA1 communication halted HW MISMATCH GIA ha rdware mismatch GIA2 communication halted A GIA mismatch has been detected where only one is WAAS capable MANIFEST GIA1 softwa communication halted re mismatch MANIFEST GIA2 softwa communication halted e mismatch The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced COM1 TEMP COM1 over temp Reducing transmitter power Reducing transmitter powe COM2 TEMP COM2 over temp f 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 G1000 system should be serviced COM1 SERVICE COM1 Return unit for repair needs service COM2 SERVICE COM2 Return unit for repair needs service The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may still be usable The G1000 system should be serviced when possible 66 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN Annunciations 8 Alerts GIA 63W MESSAGE ADVISORIES CONT Message Comments COMI PTT COM1 pu
36. Use one of the following methods to enter the reference waypoint a Turn the small FMS Knob to the left to display a list of flight plan waypoints This list is populated only when there is an active flight plan b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN Or Flight Planning 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 waypoints to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key 7 After pressing the ENT Key the cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint 8 Press the ENT Key 9 cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 10 Press the ENT Key The cursor is now placed for entering another reference waypoint if desired 11 Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 T
37. VATE 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 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 uoleiado soinjeo4 9e2uepioAy s mp old jewouqy feuonippy xipuaddy xe pul paezey unuuy Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index GPS Navigation 7 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET distance field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the 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
38. able when the G1000 is configured for a TAWS B installation 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 658 AEN Sd9 S24JV oipny dadx 93 Sjuouinajsu u102 AEN 3461 wld e uepioAy s mp old paezey Sue v uoneiedo saunyea4 junuuy jeuuouqy jeuonippy xipuaddy xe pul A Hazard Avoidance GARMIN Manual System Test Flight Instruments 1 While the TAWS Page is displayed press the MENU Key 2 Tum the small FMS Knob to select Test TAWS 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS Page When all is in working order TAWS System Test OK is heard EIS Nav Com XPDR Audio Display Terrain on the TAWS Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS Page 3 If desired press the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area AFCS GPS Nav Flight Planning Terrain Obstacle Location Terrain Obstacle above or within 100 below or above aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Hazard Avoidance Procedures Terrain Obstacle is more th
39. adio keys can be selected individually or together NAV COM TUNING 1 Press the small tuning knob to select the desired radio for tuning 2 Tum the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz 3 Press the Frequency Transfer Key to place the frequency into the active frequency field DIGITAL CLEARANCE RECORDER AND PLAYER NOTE Only the audio for the selected COM MIC Key is recorded Audio is not recorded for COM3 MIC Pressing PLAY once plays the latest recorded memory block then returns to normal operation Pressing MKR MUTE while playing a memory block stops play Pressing the PLAY Key during play begins playing the previously recorded memory block Each subsequent press of the PLAY Key begins playing the next previously recorded block Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN INTERCOM SYSTEM ICS ISOLATION Press the PILOT and or COPLT Key to select those isolated from hearing the Nav Com radios and music PILOT KEY COPLT KEY Pilot Hears Copilot Passenger ANNUNCIATOR ANNUNCIATOR Hears Hears PILOT Selected radios pilot copilot passengers music radios pilot Selected radios pilot OFF ON passengers music Selected CREW ON ON radios pilot copilot 190 00526 01 Rev B Selected radios pilot copilot passengers
40. age level ENGINE _LEAN system cvcsier assist Back F3 F V3 V3 DND MFD Softkeys ENGINE Displays the LEAN and SYSTEM softkeys LEAN Displays the engine leaning softkeys CYLSLCT Selects the desired cylinder for monitoring ASSIST Highlights the first cylinder that peaks and displays information for that cylinder BACK Press to return to the top level softkeys SYSTEM Displays fuel system softkeys 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 19 uoresado s n e 4 aoueplony SoJnpa20Jd Buiuue d AEN Sd5 yi olpny uqax 913 syu wnysu jeuonippy puezey wio gt AeN jeuuouqy Sue v unuuy gt kej 6 1 o 2 E x x pul 346 Wfl Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix 80 TRAFFIC TOPO TERRAIN AIRWAYS STRMSCP NEXRAD XM LING BACK A GARMIN DEC FUEL Press to decrease fuel quantity in 1 INC FUEL 166 GAL 194 GAL BACK gallon increments Press to increase fuel quantity in 1 gallon increments Press to reset fuel to 166 gallons Press to reset fuel to 194 gallons Press to return to the top level softkeys Enables second level Navigation Map softkeys Displays traffic information on Navigation Map Displays topographical data e g
41. aircraft and disengage the autopilot If annunciated when AP is not engaged move each half of the MET switch Separately to check if a stuck switch is causing Yaw Damper Failure System Failure AP and MET are unavailable FD may still be available 56 Failure the annunciation Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 Yaw Damper control failure 190 00526 01 Rev B A GARMIN Annunciations 8 Alerts Condition mundan Description Elevator Mistrim Up Elevator Mistrim Down Aileron Mistrim Left Aileron Mistrim Right Rudder Mistrim Left Rudder Mistrim Right Preflight Test 190 00526 01 Rev B A condition has developed causing the pitch servo to provide a sustained force Be prepared to apply nose up co upon autopilot disconnect A condition has developed causing the pitch servo to provide a sustained force Be prepared to apply nose down control wheel force upon autopilot disconnect condition has developed causing the roll servo to provide a sustained left force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance sure the slip skid indicator ntrol wheel force limits condition has developed causing the roll rvo to provide a sustained right force s centered and observe any maximum fuel imbalance limits A condition has developed causing the yaw servo to provide
42. an 1000 Black below aircraft altitude Additional Features Enable Disable Aviation Data Abnormal Operation 1 While the TAWS 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 Annun Alerts Appendix Inhibit TAWS While the TAWS Page is displayed press the INHIBIT Softkey Or Index 4 Garmin 61000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B GARMIN Hazard avoidance 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit TAWS 3 Press the ENT Key Enable TAWS While the TAWS Page is displayed press the INHIBIT Softkey Or 1 While the TAWS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable TAWS 3 Press the ENT Key NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach a LOWALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix 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
43. ck to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams aid in following ground control instructions by accurately displaying the aircraft position on the map in relation to taxiways ramps runways terminals and services 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 approach charts and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 4 e uepioAy SoJnpa20Jd Buiuue d AEN Sd5 yi olpny uqax 913 sjueumansu wio gt AeN Em jeuontppy uonesiado Jeuuouqy su jy unuuy xipuaddy x pul 346 paezey Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Avoidance Appendix Alerts Operation Index Additional Features A GARMIN FLITECHARTS FliteCharts resemble the paper version of National Aeronautical Charting Office NACO terminal procedures charts The charts are displayed w
44. ck up or down to adjust the tilt of the antenna up or down Moni tor the displayed tilt value in the TILT field of When scanning vertically a Tilt Line may be displayed to aid in positioning the tilt the antenna If the Tilt Line is not displayed perform the following steps 1 Press the MENU Key 2 Tum 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 displayed bearing value in the BEARING feld 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 44 1 Press the MENU Key 2 Tum 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 Press the VERTICAL Softkey A vertical slice of the selected area is now displayed 3 Move the Joystick right or left to move the scanned slice a few degrees right or left Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B GARMIN Hazard avoidance 4 5 Turn the Joystick to adjust the range To select a new area to be vertically scanned press the HORIZO
45. coastlines terrain rivers lakes and elevation scale on Navigation Map Displays terrain information on Navigation Map Displays airvvays on the map eycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed Displays Stormscope weather and coverage information on Navigation Map optional feature Displays NEXRAD weather and coverage information on Navigation Map optional feature Displays XM lightning information on Navigation Map optional feature Returns to top level softkeys Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN DCLTR SHVV CHRT CHKLIST 190 00526 01 Rev B Appendix Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map fea tures visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything ex cept the active flight plan When available displays optional airport and terminal procedure charts When available displays optional checklists Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 sainyea4 aoueplony seJnpe ojd ACN Sd5 5247 oipny uadx si sjuounasuy jeuonippy p ezeH Wfl uo2 AEN UTE uonejedo jJeuuouqv Sue v unuuy bd EF GARMIN Appendix s u uin s
46. d of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal isp V ARNING Because of anomalies in the earth s magnetic field operating the G1000 within the following areas could result in loss of reliable attitude and heading indications North of 70 North latitude and south of 70 South latitude An area north of 65 North latitude between longitude 75 West and 120 West An area south of 55 South latitude between longitude 120 East and 165 East CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings CAUTION The Garmin G1000 does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s 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 equ
47. de A transponder replies to interrogations Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations Automatically enters the VFR code 1200 in the U S A only Displays transponder code selection soft keys 0 7 Use numbers to enter code Removes numbers entered one at a time Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN XD ua Appendix IDENT Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen TMR REF Displays Timer References Window NRST Displays Nearest Airports Window ALERTS Displays Alerts Window MFD SOFTKEY MAP optional optional a EY EN V V3 V3 D a n Press the BACK Softkey on this level to retum to the top softkey level UY DCLTR 2 Y CI m yuma Porte sack say softkey level optional optional optional Far TERRA ARS 1 NERAD Xtra BACK 7 VF 7 VF AIRWY ON AIRWY LO system bec rue nc ruer 66 GAL isa GAL BACK ARWavHI EY v3 v3 v3 VX Press the ENGINE or BACK softkey on any level to return to the default p
48. e departure waypoint 6 Press the ENT Key 7 Repeat step number 4 5 and 6 to enter the identifier for each additional flight plan waypoint 8 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 Using the PFD 1 2 3 4 5 6 7 NOTE If a flight plan is active an additional flight plan cannot be entered using the PFD Press the FPL Key Turn the small FMS Knob to display the Waypoint Information Page Turn the small FMS Knob to enter the first letter of the destination waypoint identifier Turn the large FMS Knob to the right to move the cursor to the next character position Repeat step 3 and 4 to spell out the rest of the waypoint identifier Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint Repeat steps 3 through 6 to enter the identifier for each additional flight plan waypoint Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN Flight Planning 8 Once all waypoints have been entered press the FMS Knob to remove the cursor The new flight plan is now active INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan If required press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint i
49. e is selected Change the Stormscope Lightning Mode Between Cell and Strike 1 Select the Stormscope Page 2 Press the MODE Softkey The CELL and STRIKE Softkeys are displayed Press the CELL Softkey to display CELL data or press the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the Viewing Mode Between 360 and 120 1 Select the Stormscope Page 2 Press the VIEW Softkey The 360 and ARC Softkeys are displayed Press the 360 Softkey to display a 360 viewing area or press the ARC Softkey to display a 120 viewing area Press the CLEAR Softkey to remove all Stormscope lightning data from the display Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B amp GARMIN Avoidance XM WEATHER OPTIONAL WARNING Use of XM weather for hazardous weather penetration is not recommended Weather information provided by XM Radio Service is approved only for weather avoidance not penetration Displaying XM Weather on the Navigation Map Page 1 Press the MAP Softkey 2 Press the NEXRAD or XM LTNG Softkey to display the desired weather Press the applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF in
50. enetration Weather information provided by the GDL 69A is approved only for weather avoidance not penetration Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN Warnings Cautions amp Notes WARNING NEXRAD weather data is to be used for long range planning purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD weather data should not be used for short range weather avoidance WARNING Use of the Stormscope is not intended for hazardous weather penetration thunderstorm penetration Stormscope information as displayed on the G1000 MFD is to be used only for weather avoidance not penetration WARNING The Garmin G1000 as installed in the Beechcraft 58 G58 aircraft has a very high degree of functional integrity However the pilot must recognize that providing monitoring and or self test capability for all conceivable system failures is not practical Although unlikely it may be possible for erroneous operation to occur without a fault indication shown by the G1000 It is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely re
51. eplony SoJnpa20Jd Buiuue d AEN 5640 24V unuuy jeuuouqy jeuonippy 2 xipuaddy x pul UTE z t A o 3 Wila Flight Instruments Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Planning AFCS GPS Nav Procedures Appendix Alerts Operation Features Index amp Engine mdication syste GARMIN LEAN ENGINE DISPLAY 2328 2320 FFLOW 15 1 GPH 89 L Difference between peak EGT peak and current temperature temperature 5 cylinder Left Engine ight Engine Exhaust Gas Temperature 207 Bar Graphs Cylind n a Engine Right Engine Cylinder Head Temperature CHT Readout Bar Graphs 707 i ylinder Fight Enginc LEAN Engine Page 1 Press the ENGINE Softkey then the LEAN Softkey to display the LEAN Engine Page 2 Press the CYL SLCT Softkey to select the desired cylinder for monitoring 3 Press the ASSIST Softkey to hightlight the first cylinder that peaks Information for that cylinder is displayed The CYL SLCT Softkey becomes disabled when the ASSIST Softkey is pressed Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN ENGINE SYSTEM DISPLAY 1 Press the ENGINE Softkey then the SYSTEM Softkey to display the SYSTEM Engine Page 2 If desired use the DEC FUEL INC FUEL 166 GAL and 194 GAL softkeys to adjust the amount of fuel remaining for totalizer calculations Engine Indication System
52. es DME Information Window Wind Data Selected Heading Box Selected Course Box Transponder Status Box System Time PFD Setup Menu Windows displayed in the lower right corner of the PFD Timer References Nearest Airports Flight Plan Messages Procedures DME Tuning Barometric Minimum Descent Altitude Box A GARMIN The PFD declutters when the aircraft enters an unusual attitude Only the primary The following information is removed from the PFD and corresponding softkeys Glideslope Glide path and Vertical Deviation Indicators Altimeter Barometric Setting Selected Altitude VNV Target Altitude Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 Extreme Pitch Indication 190 00526 01 Rev B A GARMIN DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircrafts current estimated position A NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is ind
53. eviation point This altitude is and deviation guidance guidance provided as a reference Altitude does not match and is not designated to 1 the published altitude in be used in determining navigation database or no vertical speed and published altitude exists deviation guidance Small Text Altitude is not Altitude is designated The system cannot designated to be used for use in giving vertical use this altitude in in determining vertical speed and deviation determining vertical speed and deviation guidance Altitude has speed and deviation guidance Altitude has been retrieved from the guidance been retrieved from the navigation database navigation database and 1 or has been entered by is provided as a reference the pilot and matches a published altitude in the navigation database 20 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B GARMI N slight Planning FLIGHT PLANNING TRIP PLANNING 1 Turn the large FMS Knob to select the AUX page group 2 If necessary turn the small FMS Knob to select the Trip Planning Page 3 The current page mode is displayed at the top of the page AUTOMATIC or MANUAL To change the PAGE MODE press the AUTO or MANUAL Softkey 4 For Direct to planning a Press the WPTS Softkey and verify that the starting waypoint field indicates P POS present position b If necessary press the MENU Key and select Set WPT to Present P
54. formation on the Airport Information Page 1 Tum the large FMS Knob to select the WPT Page Group 2 Tum the small FMS Knob to select the Airport Information Page 3 Press the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Displaying Weather on the Weather Data Link Page 1 Tum the large FMS Knob to select the Map Page Group 2 Tum the small FMS Knob to select the Weather Data Link Page 3 Press the available softkeys to select the desired XM weather product 4 Press the LEGEND Softkey to view the legends for the selected products If necessary turn either FMS Knob to scroll through the list Press the small FMS Knob or the ENT Key to return to the map Map Panning Information Weather Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to place the panning arrow on AIRMETs TFRs METARs or SIGMETs 3 Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 3 AEN Sd9 S24JV oipny dadx Si Sjuouinajsu Ju0 AEN BITTE buluueld Wil e uepioAy s mp old paezey
55. ftware mismatch communication halted The GDL 69 has incorrect software installed The G1000 system should be serviced Hazard Avoidance GDC 74A MESSAGE ADVISORIES Features Message ADC1 ALT EC ADCI altitude error correction is unavailable Additional Comments GDC1 or GDC2 is reporting that the altitude error correction is unavailable Abnormal Operation ADC1 AS EC ADC1 airspeed error correction is unavailable a GDC1 or GDC2 is reporting that the airspeed error correction is unavailable MANIFEST GDC1 software mismatch communication halted The GDC 74A has incorrect software installed The G1000 system should be serviced Append E Index 70 Garmin 61000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN GWX 68 ALERT MESSAGES Annunciations amp Alerts Message Comments GWX CONFIG GWX config error Config service req d system should be serviced GWX 68 configuration settings do not match those of the GDU configuration The G1000 GWX FAIL GWX is inoperative The GDU is not receiving status packet from the GWX 68 or the GWX 68 is reporting a fault The GWX 68 radar system should be serviced GWX SERVICE GWX needs service Return unit for repair he GWX 68 may still be usable A failure has been detected in the GWX 68 communication halted he
56. h Pitch Hold attitude may be used to climb default PIT 8 E descend to the Selected Altitude su M Captures the Selected Altitude ALTS Capture Altitude Hold Haas Ihe qun UNS ALT Key ALT Reference gt Maintains the current aircraft R Vertical Speed vertical speed may be used to climb VS Key VS nnnn Fem descend to the Selected Altitude 22 Maintains the current aircraft 25 Flight level Change airspeed in IAS while the aircraft is IAS Hold dimbing descending to the Selected 5 Altitude 2 1 Vertical Path Tracking Captures and tracks descent legs of GDU 1045 only an active vertical profile VEN 53 VNV Target Altitude E Captures the Vertical Navigation te Capture GDU 1045 VNV Target Altitude ALTV oy i Glidepath WAAS only Cap ures and tracks the WAAS GP glidepath on approach ont HE Captures and tracks the ILS 5 Glideslope GS 32 glideslope on Disengages the autopilot and GA 58 GoAround commands a constant pitch angle GA 24 Switch and wings level ALTS armed automatically when PIT VS FLC or GA active and under VPTH when Selected Altitude 190 00526 01 Rev B A GARMIN AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds the current aircraft roll Roll Hold attitude or rolls the wings default ROL level depending on the commanded bank angle Captures and tracks t
57. h again to cycle its operation If the problem persists the G1000 system should be serviced receiver 1 and or receiver 2 The G1000 system should be serviced Return unit for repair Return unit for repair G S1 SERVICE G S1 needs service G S2 SERVICE G S2 needs service A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The G1000 system should be serviced when possible GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEA1 config error Config service req d communication halted MANIFEST GEA1 software mismatch The 1 GEA 71 has incorrect software installed The GEA1 configuration settings do not match those of backup configuration memory The G1000 system should be serviced The G1000 system should be serviced GTX 33 MESSAGE ADVISORIES Message Comments Config service req d XPDR1 CONFIG 1 config error The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced communication halted MANIFEST GTX1 software mismatch The transponder has incorrect software installed The G1000 system should be serviced 68 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN Annunciations 8 Alerts GTX 33 MESSAGE ADVISORIES CONT Message Com
58. he HDG Herang aele Selected Heading Key ids Navigation GPS m GPS Navigation VOR Enroute Arm 7 us VOR Navigation LOC No GPS VOR LOC NAV LOC Glideslope Key Captures and tracks a Navigation Backcourse localizer signal for backcourse BC approaches Approach GPS be th GPS aptures and tracks the Approach VOR selected navigation source APR zu Approach LOC Glideslope Ps VOR LOC Key 2 dl LOC Mode automatically armed Disengages the autopilot and GA Go Around commands a constant pitch GA angle and wings level No annunciation in the AFCS Status Box The acceptable bank angle range is indicated in green along the Ro Roll Hold Mode ROL Scale of the Attitude Indicator Bank Angle Flight Director Response lt 6 deg 6 to 25 deg Rolls wings level Maintains current aircraft roll attitude gt 25 deg Limits bank to 25 degrees 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 sia siu uinnsu oipny uadx U10 AEN AEN Sd5 52 Sue v uonejedo So1nje2J e uepioAy SoJnpa20Jd Buiuue d junuuy jeuuouqy jeuonippy xipuaddy x pul 346 Wfl paezey GARMIN AFCS S3u uinnsul sb 59 oipnv uddx U10 AEN S2dV AeN Sd5 Duruue d bila Blank Page 6 2 4 eouepioAy puezey SoJnjeo4 Jeuonippy uoneiedo Jeuuouqy sue v unuuy xipuaddy x pul
59. he ENT Key Or Press the Go around Button Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B GARMIN Hazardavoidance 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 qu WARNING The Stormscope system is not intended to be used for hazardous thunderstorm penetration Weather information on the G1000 MFD is approved for weather avoidance only Refer to the WX 500 Pilot s Guide for detailed operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 Press the MAP Softkey 2 Press the STRMSCP Softkey Press the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page Lightning Age Symbol Strike is less than 6 seconds old Strike is between 6 and 60 seconds old E M Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode 1 With the Weather Group selected press
60. he 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 will prevent vertical guidance to the active vertical waypoint VNV Unavailable Excessive crosstrack error The current crosstrack exceeds the limit causing vertical deviation to go invalid VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Parallel course selected A parallel course has been selected causing the vertical deviation to go invalid NO WGS84 WPT Non WGS 84 waypoint for navigation xxxx The selected waypoint poxx does not use the WGS 84 datum Cross check position with alternate navigat
61. ical limits for approved AHRS operation Heading is flagged as invalid MANIFEST GRS1 software mismatch communication halted The 1 AHRS has incorrect software installed The G1000 system should be serviced 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 69 s m ie q e uepioAvy s mp old buluueld ACN 540 S291V oipny duddx 513 Sjueuinajsu paezey wy JU05 AEN 10614 uonesado jeuuouqy x2 5 x pul Annunciations 8 Alerts GMU 44 MESSAGE ADVISORIES A GARMIN Message Flight Instruments 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 G1000 system should be serviced MANIFEST GMU1 software mismatch communication halted Nav Com XPDR Audio The GMU 44 has incorrect software installed The G1000 system should be serviced AFCS GDL 69A MESSAGE ADVISORIES Message Comments GDL69 CONFIG GDL 69 config error Config service req d GPS Nav Flight Planning GDL69 FAIL GDL 69 has failed GDL 69 configuration settings do not match those of backup configuration memory The G1000 system should be serviced A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced Procedures MANIFEST GDL so
62. icated on the G1000 by the appearance of the letters DR superimposed in yellow over the ovm aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure Also the CDI deviation bar is removed from the display Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS WAAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of accurately tracking your estimated position and consequently the system may display a path that is different than the actual movement of the aircraft Estimated position information displayed by the G1000 through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS WAAS Mode due to the lack of satellite measurements needed to determine a position Changes in wind speed and or wind direction compounds the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness
63. iewed 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 Garmin and G10009 are registered trademarks of Garmin Ltd or its subsidiaries VVATCHTM FliteChartsTM and SafeTaxiTM 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 Stormscope and SkyWatch are registered trademarks of L 3 Communications and XM is a registered trademark of XM Satellite Radio Inc January 2008 190 00526 01 Rev B Printed i n the U S A A Warnings Cautions amp Notes GARMIN WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain function The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The dis
64. ion sources 190 00526 01 Rev B 73 Garmin 61000 Cockpit Reference Guide for the Beechcraft 58 G58 s m ie q UED OAV s mp old buluueld ACN 540 S291V oipny uddx 513 Sjueuinajsu paezey wy wio gt Aen 10614 uoneiedQ jeuuouqy x2 5 x pul Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation ALARIQ Ed Index Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message Comments TRAFFIC FAIL Traffic device has failed The G1000 is no longer receiving data from the traffic system The traffic device should be serviced 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 63W ha 5 failed SCHEDULER message Message cr iteria entered by the user MAG VAR WARN Large magnetic variance Verify all course angles The GDU i exact magn nternal model cannot determine the etic variance for geographic locations near the magnetic poles Displayed magnetic Course ang heading by es may differ from the actual magnetic more than 2 74 Garmin 61000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B GARMIN 2 0 Appendix
65. ipment 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN Warnings Cautions amp Notes NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any 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 190 00526 01 Rev B Garmi
66. irport terrain database Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced The airport terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD and or PFD detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD and or PFD detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced DB MISMATCH Aviation database version mismatch Xtalk is off The PFD and MFD have different aviation database versions installed Crossfill is off Install correct aviation database version in both displays DB MISMATCH Aviation database type mismatch Xtalk is off The PFD and MFD have different aviation database types installed Ame
67. is one minute from Top of Descent Issued only when ertical navigation is enabled Procedures Vertical track Traffic Traffic Not Available ayed when a Traffic Advisory TA is issued Hazard Avoidance f P The aircraft is outside the Traffic Information Service TIS coverage area P P Additional Features Traffic Traffic Traffic Advisory System Test Passed Traffic Advisory System Test Failed ayed when a Traffic Advisory TA is issued Skywatch TAS system ayed when the TAS system passes a pilot initiated self test Abnormal Operation me ayed when the TAS system fails a pilot initiated self test ALARIQ Eed Index 98 Garmin 61000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN MFD 8 PFD MESSAGE ADVISORIES Annunciations amp Alerts Message Comments DATA LOST Pilot stored data was lost Recheck settings The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFD with preferred settings if desired XTALK ERROR flight display crosstalk error has occurred The MFD and PFD are not communicating with each other The G1000 system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair The PFD and or MFD self test has
68. ith degraded accuracy Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN Bnnunttations amp Alerts ANNUNCIATIONS amp ALERTS WARNING ANNUNCIATION Annunciation Alerts Window Message Audio Alert Text Gear up Continuous Tone received through the G1000 audio from another source Left alternator offline Repeating Tone Right alternator offline Repeating Tone Right and Left alternators offline Repeating Tone L or R fuel flow is greater than 27 4 gph Repeating Tone L or R CHT is greater than 238 deg C Repeating Tone L or R oil temp is greater than 116 deg C Repeating Tone L or R oil press is greater than 100 psi Repeating Tone L or R oil press is less than or equal to 10 psi Repeating Tone Lor R fuel qty is at zero Repeating Tone CAUTION ANNUNCIATION Annunciation Alerts Window Message Audio Alert Text Left starter relay has power applied Single Chime Right starter relay has power applied Single Chime Left bus voltage greater than 30 VDC Single Chime Right bus voltage greater than 30 VDC Single Chime Left bus voltage less than 24 V Single Chime Right bus voltage less than 24 V Single Chime Aft door not latched Single Chime Press Low Ops in icing conditions not Single Chime approved Press Low Ops in icing cond
69. ith high resolution and in color for applicable charts 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 expira tion date FliteCharts will no longer function VIEW CHARTS FROM THE NAVIGATION MAP PAGE 1 2 3 Press the SHW CHRT Softkey while viewing the navigation map This displays the airport diagram for the closest airport if available Or Move the map pointer to point to a desired point on the map and press the SHW CHRT Softkey Press the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Press the GO BACK Softkey to return to the previous page VIEW CHARTS FROM THE ACTIVE FLIGHT PLAN PAGE 1 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to select the departure airport destination airport departure arrival or approach 3 Press the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected 4 Press the GO BACK Softkey to return to the previous page CHANGE DAY NIGHT VIEW 1 While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS 2 Tum the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options
70. itions not Single Chime approved 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 s m DUEpIOAV sainparold buluueld AEN Sd5 24V oipny uadx 513 s u uin sul p ezeH UTE Jeuonippy uonejedo Jeuuouqy 5 x pul Flight Instruments Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Additional Abnormal Operation Appendia Eed Index Annunciations amp Alerts A GARMIN Annunciation Text Alerts Window Message Audio Alert L or R oil press is between 30 and 10 psi Single Chime Lor R fuel qty is less than or equal to 13 gal Single Chime Lor R alternator load exceeds 100 amps Single Chime ADVISORY ANNUNCIATION Annunciation Alerts Window Message Audio Alert Text Right Bus is tied to Left Bus None ALERT MESSAGE Alerts Window Message Audio Alert PFD FAN FAIL The cooling fan for the PFD is inoperative None MFD FAN FAIL The cooling fan for the MFD is inoperative None AVIONICS FAN The cooling fan for remote avionics is inoperative None AFCS ALERTS Condition Annunciation Description Pitch Failure PTCH Pitch axis control failure AP is inoperative Roll Failure ROLL Roll axis control failure AP is inoperative MET Switch Stuck or PTRM If annunciated when AP is engaged take Pitch Trim Axis Control control of the
71. ked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at waypoint boox Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft will penetrate the airspace within 10 minutes ARSPC NEAR Airspace near and ahead Special use airspace is near and ahead of the aircraft position ARSPC NEAR Airspace near less than 2 nm Special use airspace is within 2 nm of the aircraft position 72 Garmin 61000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN Annunciations 8 Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message Comments APR INACTV Approach is not active The system notifies the pilot that the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to t
72. large FMS Knob to highlight the desired Vspeed Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to the speed Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field Turn the small FMS Knob clockwise to ON or counterclockwise to OFF To remove the window press the CLR Key or the TMR REF Softkey Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN Flight Instruments SET BAROMETRIC MINIMUM DESCENT ALTITUDE 1 Press the TMR REF Softkey 2 Tum the large FMS Knob to highlight the OFF BARO field to the right of MINIMUMS a 3 Turn the small FMS Knob clockwise to BARO 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 To remove the window press the CLR Key or the TMR REF Softkey oipny uadx U10 AEN S24V DISPLAYING WIND DATA ACN 540 1 Press the PFD Softkey 2 Press the WIND Softkey to display wind data to the left of the HSI 3 Press one of the OPTN softkeys to change how wind data is displayed 4 To remove the Wind Data Window press the OFF Softkey buluueld 2 CHANGING HSI FORMAT 1 Press the PFD Softkey 2 Press the HSI FRMT Softkey 3 Press the 360 HSI Softkey to display the full size HSI Or Press the ARC HSI Softkey to display the arc style HS
73. ments XPDR1 SRVC XPDR1 needs service The 1 transponder should be serviced when Return unit for repair possible XPDR1 FAIL XPDR1 is inoperative There is no communication with the 1 transponder GRS 77 MESSAGE ADVISORIES Message Comments AHRS1 TAS AHRS1 not receiving airspeed the air data computer T information to augment The G1000 system shou The 1 AHRS is not receiving true airspeed from he AHRS relies on GPS the lack of airspeed d be serviced AHRS1 GPS AHRS1 using backup GPS source Primary GPS path has fa should be serviced when The 1 AHRS is using the backup GPS path iled The G1000 system possible AHRS1 GPS AHRS1 not receiving any GPS information The 1 AHRS is not recei ving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced AHRS1 GPS AHRS1 not receiving backup GPS information The 1 AHRS is not receiving backup GPS nformation The G1000 system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced AHRS1 SRVC AHRS1 Magnetic field model needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far North South no magnetic compass The aircraft is outside geograph
74. mie q UED OAV s mp old ACN 540 52 404 sia s u u nnsul paezey wy JU05 AEN 10614 uoneiedQ jeuuouqy 5 x pul Flight Instruments Additional Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Abnormal Operation Ha a o Index Annunciations amp Alerts A GARMIN MFD amp PFD MESSAGE ADVISORIES CONT Message Comments CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The G1000 system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The G1000 system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage DATABASE MESSAGE ADVISORIES The MFD voltage is low The G1000 system should be serviced Message Comments MFD1 DB ERR MFD1 aviation database error exists PFD1 DB ERR PFD1 aviation database error exists The MFD and or PFD detected a failure in the aviation database Attempt to reload the aviation database If problem persists the G1000 system should be serviced MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists The MFD and or PFD detected a failure in the basemap database MFD1 DB ERR MFD1 terrain database error exists
75. n G1000 Cockpit Reference Guide for the Beechcraft 58 G58 A Cautions amp Notes GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 658 190 00526 01 Rev B A GARMIN Change Summary 190 00526 01 RevA Changed to smaller format Added Airways WAAS VNAV and Charts Updated G1000 System Messages Added other GDU 8 10 parameters Revision Date of Revision Affected Pages January 2008 76 77 Removed FD Formatting feature 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 RR 1 A GARMIN Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 658 190 00526 01 Rev B A GARMIN ble of Contents FLIGHT INSTRUMENTS 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg 1 Change Altimeter Barometric Pressure Setting Units 1 Change Navigation Sources sssssssseeeenennn nnns 1 Enable Disable OBS Mode While Navigating with 6 5 5 2 Generic TIGE rmn ho qas ica in ice n a 2 Configure Vspeed Bugs Individually sss 2 Set Barometric Minimum Descent Altitude sss 3 Displaying Wind Data 3 Changing HSI Format nennen 3 ENGI
76. nce ACTIVATE AN ARRIVAL 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 desired waypoint within the arrival 4 Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE NOTE If certain GPS parameters WAAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT APPROACH 32 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B GARMIN X C 8 Procedures Press the ENT Key A list of available approaches for the destination airport is displayed 4 Turn either FMS Knob to highlight the desired approach n VVAAS capable systems the VVAAS channel and D for the selected approach procedure are displayed in the APPROACH CHANNEL field 5 Press the ENT Key A list of available transitions for the selected approach procedure is now displayed 6 Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course 7 Press the ENT Key LOAD or ACT
77. nges have been made press the FMS Knob to remove the Cursor INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the desired flight plan 5 Press the INVERT Softkey Invert and activate stored flight plan is displayed 6 With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location COPY A FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be copied 5 Press the COPY Softkey A Copy to flight plan confirmation window is displayed 6 With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key 28 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN Flight Planning DELETE A FLIGHT PLAN 1 2 3 4 5 6 Press the FPL Key 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 deleted
78. now displayed on the map Traffic Advisory System TAS Optional System Self Test 1 Set the range to 2 6 nm 2 Press the STANDBY Softkey 3 Press the TEST Softkey 4 Self test takes approximately eight seconds to complete When completed successfully traffic symbols are displayed and a voice alert Traffic Advisory System Test Passed is heard If the self test fails the system reverts to Standby Mode and a voice alert Traffic Advisory System Test Failed is heard Displaying Traffic on the Traffic Map Page 1 Tum the large FMS Knob to select the Map Page Group 2 Tum the small FMS Knob to select the second rectangular page icon 3 Press the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Press the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field 5 Press the STANDBY Softkey to place the system in the Standby Mode STANDBY is 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 Displaying Traffic on the Navigation Map 1 Ensure TAS is operating With the Navigation Map displayed press the MAP Softkey 2 Press the TRAFFIC Softkey Traffic is now displayed on the map Garmin G1000 Cockpi
79. on ENTER A TRANSPONDER CODE 1 Press the XPDR Softkey to display the transponder mode selection softkeys 2 Press the CODE Softkey to display the transponder code selection softkeys for digit entry 3 Press the digit softkeys to enter the code in the code field When entering the code the next key 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 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 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 sjueumansu S24JV oipny uadx Si UI0JNeN Sue v uonejedo saunqea4 aoueplony Buiuue d AEN 5640 unuuy jeuuouqy jeuonippy paezey xipuaddy xepu 3461 Flight Instruments Nav Com AFCS XPDR Audi Flight Planning Abnormal Additional Hazard Avoidance Annun EIS GPS Nav Procedures Appendix Alerts Operation Features Index A Nav Com XPDR Audio Panel GARMIN SELECTING A NAV RADIO 1 Press the CDI Softkey to select NAV1 VOR1 LOC1 or NAV2 VOR2 LOC2 2 Pressing the NAV1 NAV2 DME or ADF Key selects and deselects the navigation radio audio source All r
80. osition to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field d Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint Or For point to point planning a Enter the identifier of the starting waypoint b Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again enter the identifier of the ending waypoint d Press the ENT Key to accept the waypoint Or For flight plan leg planning a Press the FPL Softkey at the bottom of the display b Turn the small FMS Knob to select the desired flight plan already stored in memory by number Turn the large FMS Knob to highlight the LEG field d Turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 21 oipny dadx 53 Sjuouinajsu U10 AEN aui S24V s mp old Buruuejd ACN Sd5 nubi Sue v uonejedo sainqea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 5 6 7 8 9 A GARM
81. played minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74A Air Data Computer or other altimeters in aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING XM Weather should not be used for hazardous weather p
82. r 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 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 49 syay uone1ado EGIPEN 9e2uepioAy SoJnpao20Jd Duruue d ACN Sd5 52 444 Sjueuinajsu junuuy jpuuouqv a JU105 AEN xipuaddy xe pul 346 2 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 50 A GARMIN Select an Available Channel within the Selected Category 1 2 3 While on the XM Radio Page press the CHNL Softkey Press the CH Softkey to go up through the list in the Channel Box or move down the list with the CH Softkey Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels With the desired channel highlighted press the ENT Key Entering a Channel Directly 1 2 3 4 While on the XM Radio Page press the CHNL Softkey Press the DIR CH Softkey The channel number in the Active Channel Box is highlighted Press the numbered softkeys located on the bottom of the display to directly select the desired channel number Press the ENT Key to activate the selected channel Assigning Channel
83. re has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced Return unit for repair SERVICE NAV2 needs service Return unit for repair NAV1 SERVICE NAV1 needs service A failure has been detected in the NAV1 Return unit for repair and or NAV2 receiver The receiver may still NAV2 be available The G1000 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 G1000 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 G1000 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 G1000 system should be serviced when possible GIA 63W MESSAGE ADVISORIES Message Comments GIA1 CONFIG G A1 config error Config service req d GIA2 CONFIG GIA2 config error Config se
84. ricas European etc Crossfill is off Install correct aviation database type in both displays 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 s mie q UED OAV s mp old buluueld ACN 540 S291V 04 sia Sjueuinajsu paezey wy wio gt AeN 10614 uoneiedQ jeuuouqy 2d cae x pul Flight Instruments Additional Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Abnormal Operation Eed Index Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message Comments DB MISMATCH Terrain database version mismatch The PFD and MFD have different terrain database versions installed Install correct terrain database version in both displays DB MISMATCH Terrain database type mismatch The PFD and MFD have different terrain database types installed Install correct terrain database type in both displays DB MISMATCH Obstacle database version mismatch The PFD and MFD have different obstacle database versions installed Install correct obstacle database version in both displays DB MISMATCH Airport Terrain database mismatch The PFD and MFD have different airport terrain databases installed Install correct airport terrain database in both displays GMA 1347 MESSAGE ADVISORIES Message Comments
85. rmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 s m ie q uepI ony s mp old buluueld ACN 540 S291V oipny uddx 513 Sjueuinajsu paezey wy wio gt Aen 10614 jeuonippy uoneiedQ jeuuouqy d 5 x pul Flight Instruments Additional Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Abnormal Operation Hagamik Ec Index Annunciations amp Alerts A GARMIN GIA 63 MESSAGE ADVISORIES CONT Message Comments Return unit for repair Return unit for repair 0 1 SERVICE COM1 needs service 0 2 SERVICE 2 needs service The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may still be usable The G1000 system should be serviced when possible is stuck COM1 PTT COM1 push to talk key is stuck transfer key is stuck COM2 PTT COM2 push to talk key COM1 RMT XFR COM1 remote transfer key is stuck COM2 RMT XFR COM 2 remote The COM1 and or COM2 external push to talk Switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced The COM1 and or COM2 transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced RAIM UNAVAIL
86. rn the large FMS Knob to highlight the desired flight plan 4 Press the EDIT Softkey 5 Turn the large FMS Knob to place the cursor in the desired location Jeuonippy paezey s m ie q uonejado jeuuouqy 6 Enterthe changes then press the ENT Key 7 Press the FMS Knob to return to the Flight Plan Catalog Page Sue v unuuy DELETE A VVAYPOINT FROM THE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor xipuaddy Or for a stored flight plan a Press the FPL Key on the MFD xe pul 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 21 Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning 2 3 4 5 A GARMIN b Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor d Turn the large FMS Knob to highlight the desired flight plan e Press the EDIT Softkey Turn the large FMS Knob to highlight the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key Once all cha
87. rvice req d The GIA1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 65 So1njeo4 s mp old buluueld ACN 540 52 404 sia Sjueuuinajsu paezey wy wio gt AeN 10614 uoneiedQ jeuuouqy x2 5 x pul Flight Instruments Additional Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Abnormal Operation Hg Index Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message error Config service req d GIA1 CONFIG G A1 audio confi G error Config service req d A2 CONFIG GIA2 audio confi Comments The GIA1 and or GIA2 have an error in the audio configuration The 61000 system should be serviced too low GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature temperature GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be serviced Return the unit for repair GIA1 SERVICE GIA1 needs service
88. s inserted before the highlighted waypoint Turn the small FMS Knob The Waypoint Information Window is now displayed Enter the new flight plan waypoint by one of the following a b a b d a b o d e Enter the user waypoint identifier facility or city Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the NRST airport waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Press the ENT Key again to accept the waypoint 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 25 oipny dadx 53 Sjuouinajsu U10 AEN aui S24V s mp old Buruuejd ACN Sd5 nubi Sue v uonejedo So1nje2J e uepioAy unuuy jeuuouqy jeuonippy paezey xipuaddy xe pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning A GARMIN ENTER AN AIRWAY IN A FLIGHT PLAN 1 2 3 4 5
89. scope lightning data on the Inset Map within a 200 nm radius of the aircraft NEXRAD Displays NEXRAD weather and coverage information on Inset Map optional feature XM LING Displays XM lightning information on Inset Map optional feature optional C ro oss 1 Leo xen Lev 1 fene nest n FE v n mn FE n n BRG2NAVI IBRG2 GPS IJ C ees L ea F3 V3 F3 F3 nm nm n5 o n n 74 EE 189 pes E EEE Trsee yaram ou nn rom Press the BACK Softkey to return to the top level softkeys L pem Lorna os or Ld J fates EY V3 VP3 PF o3 E58 NUNU 058 75 Dn nm 76 3 PFD Configuration Softkeys Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A GARMIN PFD DFLTS WIND OPIN I OPTN 2 OPTN 3 OFF DME BRGI HSI FRMT 360 HSI ARC HSI BRG2 ALT UNIT METERS IN HPA STD BARO 190 00526 01 Rev B Appendix Displays second level softkeys for ad ditional PFD configurations Resets PFD to default settings including changing units to standard Displays softkeys to select wind data parameters Longitudinal and lateral components Total direction and speed Total direction with head and crosswind speed components Information not displayed Displays the DME Information Window Cycles the Bearing 1 Information Win dow through NAV1 or GPS waypoint identifier and GPS derived distance information and ADF frequency Di
90. sh to talk key is stuck is stuck COM2 PTT COM2 push to talk key The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced COM1 RMT XFR COM1 remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck The COM1 and or COM2 transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced LOI GPS integrity lost Crosscheck with other NAVS GPS integrity is insufficient for the current phase of flight GPS NAV LOST Loss of GPS navigation Insufficient satellites f tion due to insufficient eV Loss of GPS navig satellites GPS NAV LOST Loss of GPS navigation Position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to position error Loss of GPS navigation due to GPS failure Abort approach ABORT APR Loss of GPS navigation Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Use LNAV minima when approach is downgraded TRUE APR True north approach Change HDG reference to TRUE Displayed after passing the first waypoint of a true north approach when the nav angle is set
91. splays the HSI formatting softkeys Displays the HSI in a 360 degree format Displays the HSI in an arc format Cycles the Bearing 2 Information Win dow through NAV2 or GPS waypoint identifier and GPS derived distance information and ADF frequency Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter in meters Press to display the BARO setting as inches of mercury Press to display the BARO setting as hectopacals Sets barometric pressure to 29 92 in Hg 1013 hPa 7 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 So1nje2J e uepioAy SoJnpa20Jd Buiuue d AEN Sd5 2 olpny uqax sia sjueumansu jeuonippy paezey bil wio gt AeN 4613 uoesado jeuuouqy sue v unuuy z psg Annun Abnormal Additional Hazard Flight Nav Com Fight Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Appendix Index Appendix A GARMIN optional mr K s Ce Lee X998 H sir fer Wer WERTS XPDR 78 n Press the BACK Softkey to return to the top level softkeys 3E EIE IE AES 7 Tom Tser TE Yaram Press the BACK Softkey to return to the previous level softkeys Transponder Softkeys STBY ON ALT GND VFR CODE 0 7 BKSP Displays transponder mode selection softkeys Selects Standby Mode transponder does not reply to any interrogations Selects Mo
92. sponsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the Beechcraft 58 G58 Pilot s Operating Handbook POH Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G1000 to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 A Warnings Cautions amp Notes GARMIN WARNING The illustrations in this guide are only examples Never use the G1000 to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo WARNING Lamp s inside this product may contain mercury HG and must be recycled or dispose
93. ssusess 75 MED Softkey ccccccccccssssssssssssssssssscssssvsssssesssssssssssesssssssssscesssssssssscesssssssssecesssssssvnsess 79 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 A Table of Contents GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B GARMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG 1 Press the PFD Softkey 2 Press the STD BARO Softkey to set standard barometric pressure CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Press the PFD Softkey to display the second level softkeys 2 Press the ALT UNIT Softkey 3 Press the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Press the HPA Softkey to display the barometric pressure setting in hectopascals 4 Press the BACK Softkey to return to the top level softkeys CHANGE NAVIGATION SOURCES 1 Press the CDI Softkey to change from GPS to VOR1 or LOC1 This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD 2 Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the light blue tuning box over the NAV2 standby frequency 3 Press the CDI Softkey a third time to ret
94. t Instruments Additional Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Abnormal Operation Append rd Index Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message Comments TIMER EXPIRD Timer has expired DB CHANGE Database changed Verify user modified procedures The system notifies the pilot that the timer has expired This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an aviation 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 aviation database This alert is issued only after an aviation database update Verify use of airways in stored flight plans and reload airways as needed FPL TRUNC Flight plan has been truncated This occurs when a newly installed aviation database eliminates an obsolete approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach LOCKED FPL Cannot navigate locked flight plan This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove loc
95. t Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B GARMIN Hazard Avoidance TERRAIN AND OBSTACLE PROXIMITY NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south Displaying Terrain and Obstacles on the Terrain Proximity Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the last rectangular page icon 3 If desired press the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey is pressed a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below or above aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed press the MAP Softkey 2 Press the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY OPTIONAL NOTE Terrain data is not displayed vvhen the aircraft latitude is greater than 75 degrees north or 60 degrees south A NOTE TAWS operation is only avail
96. the ENT Key The cursor flashes on STRMSCP LING 2 Tum the large FMS Knob to select STRMSCP MODE 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 35 s u uinnsu 3 S24V oipny uddx 5 JU105 AEN ACN Sd buluueld s m ie q s y uonesado unuuy euuougy xipuaddy x pul 3461 e uepioAy s mp old paezey Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN 36 3 Turn the small FMS Knob to display the Cell Strike window 4 Turn either FMS Knob to select Cell or Strike Press the ENT Key 5 Push the FMS Knob to return to the Navigation Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page 1 Turn the large FMS Knob until the Map Page group is selected 2 Turn the small FMS Knob until the Stormscope Pag
97. the cursor 3 Turn the large FMS Knob to place the cursor in the SECTOR SCAN field 45 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 AEN Sd5 24V oipny uadx s z sjueumasuj JU05 AEN 10614 Duruue d s mp old paezey Sue v uoneiedo SoJnjeaJ junuuy jeuuouqy jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN 4 Turn 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 Antenna Stabilization 1 To activate or deactivate the antenna stabilization press the MODE Softkey 2 Press the STAB ON Softkey to activate antenna stabilization or press the STAB OFF Softkey to deactivate The current stabilization condition is shown in the upper right of the weather radar display Weather Attenuated Color Highlight WATCH To activate or deactivate the Watch feature press the WATCH Softkey This feature is only available in the Horizontal Scan Mode Weather Alert To activate or deactivate Weather Alert press the WX ALRT Softkey Activating and deactivating also enables or inhibits the alert on the PFD
98. 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 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 AEN Sd5 24V oipny uadx s z sjueumasuj JU05 AEN 10614 ni SeJnpa20Jd Sue v uonejedo saunqea4 e uepioAy unuuy jeuuouqy jeuonippy puezey xipuaddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures GARMI N 4 Turn the large FMS Knob to highlight the desired arrival 5 Press the ENT Key A list of transitions is displayed for the selected arrival 6 Turn either FMS Knob to select the desired transition 7 Press the ENT Key A list of runways may be displayed for the selected arrival 8 Turn the large FMS Knob to highlight the desired runway 9 Press the ENT Key 10 With LOAD highlighted press the ENT Key 11 The arrival becomes part of the active flight plan 12 If an altitude associated with a waypoint in an arrival procedure is to be used to calculate vertical guidance perform the following steps a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to highlight the desired waypoint altitude Press the ENT Key to designate the altitude for use in giving vertical guida
99. to AUTO Return unit for repair GPS1 SERVICE GPS1 needs service Return unit for repair 190 00526 01 Rev B GPS2 SERVICE GPS2 needs service A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced 67 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 S91njeo4 e uepioAvy s mp old buluueld ACN 540 S291V oipny duddx sia Sjueuinajsu paezey Wila wio gt AeN 10614 jeuonippy uoneiedQ jeuuouqy x2 5 xepu Flight Instruments Additional Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Abnormal Operation enero Index Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message Comments Return unit for repair Return unit for repair NAV1 SERVICE NAV1 needs service NAV2 SERVICE NAV2 needs service A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G1000 system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck 6 51 FAIL G S1 is inoperative A failure has been detected in glideslope 6 52 FAIL G S2 is inoperative The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switc
100. to but not including the FAE The FAF is always a reference only altitude and cannot be designated unless the selected approach does not provide vertical guidance In this case the FAF altitude can be designated Altitudes associated with arrival procedures are manually designated This means the system does not use the altitudes loaded with the arrival for giving vertical speed and deviation guidance until designated to do so by the pilot Note that these altitudes are initially displayed as white text These altitudes may be designated by placing the cursor over the desired altitude and pressing the ENT Key After designation the text changes to light blue Altitudes that have been designated for use in vertical guidance may also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key The altitude is now displayed only as a reference It will not be used to give vertical 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 the Altitude has been entered The system cannot System estimating the by the pilot Altitude use this altitude in altitude of the aircraft as it is designated for use determining vertical passes over the navigation in giving vertical speed speed and d
101. tudes 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 KIXD KDFW Ir i KARLA AYIRIR B la U aree White COVIE 221 9 NM 12400FT Pn LEMYN 220 g m 99002 Laree Lig Approach KDFW RNAV 17LsPs Bine Text RIVET iaf 259 18 8NM aag Small Lig DRAAK 176 3 3MM Blue Text INWOD 176 3 2MM MENOL faf 176 39 zamer De Subdued RW17L map 1767 5 3MM Small White Text 99 FT 174 0 8NH kenas s with Altitude POLKE Restriction Bar S L M Cross AT or ABOVE 5 000 fi VAC B Cross AT 2 300 ft Cinn 1416 Cross AT or BELOW 3 000 ft Altitudes associated with approach procedures are auto designated This means the system automatically uses the altitudes loaded with the approach for giving vertical 19 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 513 6 15 sub oipny uadx U10 AEN Sue v uonejedo saunqea4 aoueplony SoJnpa20Jd Buiuue d jeuuouqy jeuonippy paezey 461 unuuy xipuaddy xe pul Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index GPS Navigation GARMI N speed and deviation guidance Note these altitudes are displayed as light blue text up
102. ul sub 59 oipnv uadx 010 AEN 52 AeN 5492 Duruue d bila Blank Page 6 2 4 eouepioAy puezey SoJnjeo4 Jeuonippy uoneiedo Jeuuouqy sue v unuuy xipuaddy Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 658 190 00526 01 Rev B 82 A GARMIN A Activate a flight plan 18 Active Channel 49 ADF 9 10 52 77 AHRS 69 70 Airways 80 Alert messages 71 ALT 40 Altitude mode 40 Altitude volume 40 Antenna stabilization 46 Antenna tilt 44 AP 56 ASSIST 6 Audio panel controls NAV1 NAV2 10 Autopilot 57 Barometric Altitude Minimums 3 Barometric pressure 77 Bearing line 44 45 46 C CDI 1 10 73 Cell 35 36 Cell mode 36 Channel Presets 50 ChartView 47 61 Clearance player 10 Clearance Recorder 10 Code selection softkeys 9 COM 9 10 51 CYL SLCT 6 D DCLIR Softkey 47 Dead Reckoning 53 Index Declutter 52 75 81 Direct to 17 DME 9 10 DR mode 53 54 E Edit a flight plan 27 F FD 56 Flight Director 13 15 FliteCharts 47 48 Frequency Transfer 10 G Gain 45 Ground mapping 45 H HF 9 Horizontal scan 45 Inhibit 42 Inhibit TAVVS 43 Inset Map 75 76 J Jeppesen 47 L Lightning 35 36 76 M Map panning 37 Message advisories 59 62 64 65 69 74 Index 1 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 sy jy uone1ado S9Jnjeo4 92uepioAy s mp old bul
103. urn 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 Tur the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn the small FMS Knob to highlight the desired waypoint 6 Press the DELETE Softkey 7 The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 23 oipny dadx 93 Sjuouinajsu U10 AEN aui S24V s mp old Buruuejd ACN Sd5 nubi Sue v uonejedo So1nje2J e uepioAy unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A NEW FLIGHT PLAN 24 NOTE When creating a new flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Using the MFD 1 Press the FPL Key 2 Tum the small FMS Knob to display the Flight Plan Catalog Page 3 Press the NEW Softkey to display a blank flight plan for the first empty storage location 4 Turn the small FMS Knob to display the Waypoint Information Window 5 Enter the identifier of th
104. urn to GPS 190 00526 01 Rev B Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 Sue v uonejedo So1nje2J aoueplony SoJnpa20Jd Buiuue d AEN Sd5 yi olpny uqax 513 unuuy jeuuouqy jeuonippy paezey BITTE u102 AEN xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Flight Instruments GARMIN ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 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 2 3 Press the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted Turn the small FMS Knob to display the UP DOWN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it starts counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window CONFIGURE VSPEED BUGS INDIVIDUALLY 1 2 3 4 5 6 Press the TMR REF Softkey Turn the
105. uueld AEN Sd5 241V oipny uddx SI3 Sjueuuinajsu junuuy jJeuuouqgy Jeuonippy 2 Wil JUI05 AEN Juil xipu ddy Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts E Appendix Index MET 56 METAR 37 Minimums 58 Mistrim 57 MKR MUTE 10 Mode S 78 Mode selection softkeys 9 Multi Function Display MFD Softkeys 79 N NACO 48 NAV 10 NAV1 1 10 NAV2 1 10 Navigation database 19 20 NEXRAD 37 38 76 80 0 OBS 2 Obstacles 62 66 Overspeed Protection 14 R Reversionary mode 51 S SafeTaxi M 47 Sector scan 45 46 STAB 46 Standby 43 Store Flight Plan 27 Stormscope lightning data 35 36 76 Strike 35 Strike mode 36 Index 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 A GARMIN T TA 58 TAF 37 TAS 40 58 69 TAWS 41 42 43 58 TAWS B 41 Terrain 41 62 76 80 Tilt line 44 Topographical data 76 80 Traffic 35 39 76 80 Traffic Advisory 58 Traffic advisory 39 Traffic map page 39 40 41 Transponder 9 78 79 V Vertical deviation guidance 20 Vertical speed guidance 20 Vertical track 58 VNV 17 52 73 Vspeed 2 W WAAS 33 66 WATCH 46 Weather Attenuated Color Highlight 46 Weather data link page 37 Weather radar 43 Wind data 77 X XM lightning 76 80 XM weather 37 Y Yaw damper 56 190 00526 01 Rev B A G
106. vate an Approach Procedure sss 32 Activate An Approach in the Active Flight Plan 33 Activate a Vector to Final Approach Fix sss 33 Activate A Missed Approach in the Active Flight Plan 34 HAZARD 35 Customizing the Hazard Displays on the Navigation 35 STORMSCOPE Optional 0 cccccccccsssussssssssssssssessssssssssssessssssssesssssssssseessasssssseeseaen XM Weather Optional Traffic Systems eid mera P n e nah Terrain And Obstacle Proximity Terrain Awareness amp Warning System TAWS Display Optional 41 Airborne Color Weather Radar sse 43 ADDITIONAL FEATURES nnne SafeTaxi TM scs into ChartView sss FliteCharts View Charts from the Navigation Map 48 View Charts from the Active Flight Plan Page 48 Change Day Night View sssssseee nnne 48 XM Radio Entertainment sssssseeeennnnns 49 ABNORMAL OPERATION 0 51 Reversionary Mode Abnormal COM Operation seen 51 Garmin G1000 Cockpit Reference Guide for the Beechcraft 58 G58 190 00526 01 Rev B A

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