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Garmin SA01456Wi_D Cockpit Reference Guide

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1. csssssssssssesssseeseunssstensas 9 Flight Director Activation ssssssennnnnnnnnnes 9 Vertical Modes aidera c ete Id ce t o 0 Lateral Modes 1 GPS NAVIGATION aote ED otl bo atii dele 3 Direct to Navigation sssssssseeee nennen 3 Activate a Stored Flight Plan 4 Activate a Flight Plan Leg 4 Stop Navigating a Flight Plan 5 Vertical Navigation VNAV ssssseeen nnne 5 FLIGHT PLANNING n toe orta ettam d erae 9 Weight Planning ssssssseenenennnnnennnnnnnnnnnnnns 9 Trip Planning treten cnt temi tne Gn man 9 Create a User Waypoint Defined by Latitude amp Longitude 21 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi Table of Contents GARMI N Create a User Waypoint Defined by Radials from Other Waypoints 22 Create a User Waypoint Defined by a Radial amp Distance from Another Waypoint 24 Delete a User Waypoint Create a Flight Plan Import a Flight Plan from an SD Card Insert a Waypoint in the Active Flight Plan Enter an Airway in a Flight Plan Invert An Active Flight Plan Remove a Departure Arrival Approach or Airway from a Flight Plan 29 Store a Flight Plan toto eterne teta ene Edit a Stored Flight Plan Delete a Waypoint from the Flight Plan sss Invert and Activate a Stored Flight Plan
2. Turn the large FMS Knob to select the desired waypoint d Press the ENT Key ENTER AN AIRWAY IN A FLIGHT PLAN 28 1 2 3 4 5 6 1 Press the FPL Key on the Control Unit Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint after the desired airway entry point If this waypoint is not a valid airway entry point a valid entry point should be entered at this time Turn the small FMS Knob one click clockwise and select the LD AIRWY Softkey or press the MENU Key and select Load Airway required on the PFD The Select Airway Page is displayed The LD AIRWY Softkey or the Load Airway menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown first in the list followed by all altitude airways and then high altitude airways Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted Press the ENT Key The system returns to editing the flight plan with the new airway inserted Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMIN Flight Planning INVERT AN ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 Press t
3. WARNING The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74B Air Data Computer or other altimeters in the aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Do not rely solely upon the display of traffic information for collision avoidance maneuvering The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot s responsibility to see and avoid other aircraft 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi amp Warnings Cautions amp Notes GARMIN WARNING Do not rely solely upon the display of traffic information to accurately depict all of t
4. With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic will now be displayed on the map TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY 46 NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Manual System Test 1 2 3 While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Test TAWS System Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK will be heard Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN Display Terrain and Obstacles on the TAWS B Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS B Page 3 f desired select the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstacle
5. Dun PIE xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix MEN Index Annunciations amp Alerts GRS 77 MESSAGE ADVISORIES A GARMIN Message AHRS1 TAS AHRS1 not receiving valid airspeed Comments The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The system should be serviced AHRS2 TAS AHRS2 not receiving valid airspeed The 2 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The system should be serviced AHRS1 GPS AHRS1 using backup GPS source The 1 AHRS is using the backup GPS path Primary GPS path has failed The system should be serviced when possible AHRS2 GPS AHRS2 using backup GPS source The 2 AHRS is using the backup GPS path Primary GPS path has failed The system should be serviced when possible AHRS1 GPS AHRS1 not receiving any GPS information The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The system should be serviced AHRS2 GPS AHRS2 not receiving any GPS information The 2 AHRS is not receiving any or any useful GPS information Check AFMS limitations The system should be serviced AHRS1 GPS AHRS1 not receiving backup GPS
6. field Additional Features Turn the small FMS Knob to select the desired checklist and press the ENT Key The selected checklist item is indicated with white text surrounded by a white box Press the ENT Key or select the CHECK Softkey to check the selected checklist item The line item turns green and a checkmark is placed in the associated box The next line item is automatically selected for checking Either FMS Knob can be used to scroll through the checklist and select the desired checklist item Press the CLR Key or select the UNCHECK Softkey to remove a check mark from an item When all checklist items have been checked Checklist Finished is displayed in green text at the bottom left of the checklist window and GO TO NEXT CHECKLIST is highlighted If GO TO NEXT CHECKLIST is selected prior to checking all the checklist items CHECKLIST NOT FINISHED will be displayed in yellow text 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 57 Sa1npa oJd Buruue d AEN Sd5 24V oipny udax sjueumansu JWI05 NEN aouepioay puezey xipuaddy su jy unuuy EE Jeuonippy xopu 36114 34614 Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features GARMIN 58 eco 9 Press the ENT Key If GO TO NEXT CHECKLIST is displ
7. page mode ground speed is provided by the system oipny uddx U105 AEN 8 The flashing cursor moves to the fuel flow field Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system S2dV 9 Theflashing cursor moves to the fuel onboard field Modify the fuel onboard Press the ENT Key when finished In AUTOMATIC mode fuel onboard is provided by the entry made on the Weight Planning Page The flashing cursor moves to the calibrated airspeed CALIBRATED AS field Enter the calibrated airspeed Press the ENT Key when finished Note that in AUTOMATIC page mode calibrated airspeed is provided by the system The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by the system AEN Sd5 10 11 12 The flashing cursor moves to the barometric setting PRESSURE field Enter the desired baro setting Press the ENT Key when finished Note that in AUTOMATIC page mode the baro setting is provided by the setting entered on the PFD The flashing cursor moves to the air temperature TOTAL AIR TEMP field Enter the desired air temperature Press the ENT Key when finished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature ad e a D 2 m o v a
8. serviced 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 85 eouepioAy seinpa2oJd Buruue d AEN Sd5 241V oipny uddx Sjueuinjjsu paezey 1ufi4 U405 AEN Wij soinjes Jeuonippy xipuaddy xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix IE Index Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message Comments FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63 W has failed MAG VAR WARN Large magnetic variance Verify all course angles The GDU s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may differ from the actual magnetic heading by more than 2 SVS SVS DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVS SVS DISABLED Terrain DB resolution too low SCHEDULER f message Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed Message criteria entered by the user CHECK CRS Database course for LOCI LOC ID is CRS Selected course for LOC1 differs f
9. GPS integrity is insufficient for the current phase of flight 74 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 190 00664 02 Rev B A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT Message COM1 RMT XFR COM remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck Comments The COM1 and or COM transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its operation If the problem persists the system should be serviced COM1 CONFIG COM config error Config services req d error Config services req d COM2 CONFIG COM config COM1 and or COM2 configuration settings do not match backup configuration memory The system should be serviced GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by SBAS is unavailable use LNAV only minimums TRUE APR True north approach Change HDG reference to TRUE
10. Index A Appendix GARMIN Loading Garmin Database Updates 96 1 2 3 4 5 6 7 8 9 10 11 12 w With system power OFF remove the MFD database card from the bottom card slot of the MFD Update the Garmin databases on the MFD card Insert the MFD database card into the bottom card slot of the MFD Apply power to the system check that the databases are initialized and displayed on the power up screen When updating the terrain and FliteCharts databases a Verifying message may be seen If this message is present wait for the system to finish loading before proceeding to step 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete being displayed Remove and reapply power to the system Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct database cycle information is shown for each database for each display Loading the Active Navigation Database 1 2 NOTE Loading the Naviga
11. Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The system should be serviced PFD2 VOLTAGE PFD2 has low voltage Reducing power usage The PFD2 voltage is low The system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The system should be serviced DATABASE MESSAGE ADVISORIES Message Comments MFD1 DB ERR MFD1 aviation database error exists PFD1 DB ERR PFD1 aviation database error exists PFD2 DB ERR PFD2 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 system should be serviced 68 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 190 00664 02 Rev B A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists PFD2 DB ERR PFD2 basemap database er
12. Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand 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 equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation
13. There are no indications marking the pitch ESP engage and disengage limits in these nose up nose down conditions Procedures Hazard Avoidance I 2 3 zi lt Annun Alerts Appendix High Airspeed Protection Index Exceeding Vmo or Mmo will result in ESP applying force to raise the nose of the aircraft When the high airspeed condition is remedied ESP force is no longer applied 56 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN ELECTRONIC CHECKLISTS The system accesses the checklists from an SD card inserted into the card slot If the SD card contains an invalid checklist file or no checklist the Power up Page messages display Checklist File Invalid or Checklist File N A not available and the CHKLIST Softkey is not available The following colors are used for checklist items e Light Blue Items not selected or Gray General notes checked White Item is selected Yellow Caution notes Red Warning notes Green Item has been checked Accessing and Navigating Checklists 1 2 3 4 5 6 1 From any page on the MFD select the CHKLIST Softkey or turn the large FMS Knob to select the Checklist Page Turn the large FMS Knob to select the GROUP field Turn the small FMS Knob to select the desired procedure and press the ENT Key Turn the large FMS Knob to select the CHECKLIST
14. With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMIN Flight Planning Or A a Turn the small FMS Knob to the left Initially a flight plan waypoint list E is displayed S b Turn the small FMS Knob to the right to display the RECENT T waypoints ES Ja Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint 12 Press the ENT Key 13 The
15. amp ALERTS 59 G1000 System Annunciations sen 59 Advisory Annunciations seen Message Advisory Alerts Comparator Annunciations ssssssseee nnn Reversionary Sensor Annunciations AFCS Alerts ee trata TAWS Alerts Aural Alerts Flight Plan Import Export Messages MFD amp PFD Message Advisories sssssssss Database Message Advisories GMA 1347D Message Advisories ssssssssseene GIA 63W Message Advisories sss GEA 71 Message Advisories GTX 33 Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories GDL 69A Message Advisories sse GWX 68 Alert Messages nen GDC 74B Message Advisories GCU 475 Message Advisories GMC 710 Message Advisories seen Miscellaneous Message Advisories ssssssss APPENDIX ctrca a t nete aot ue tton eain eat PFD Softkey Map MFD Softkey Map Loading Updated Databases 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi il Table of Contents GARMI N Blank Page iv Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft COOA GT GTi 190 00664 02 Rev B GARMIN Flight Instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING EL a E g E 3 o 3 FA a Turn the BARO Knob to select the desired setting oipn
16. amp 3 Rudder Mistrim A condition has developed causing the yaw servo to E Left RUD provide a sustained force Rudder Mistrim A condition has developed causing the yaw servo to providea Right RUD sustained force 2 Preflight Test Performing preflight system test Upon completion of the PETS test the aural alert will be heard PFT Preflight system test has failed TAWS ALERTS E PFD MFD E ee Alert Type TAWS B Page Aural Message s Pop Up Alert E Annunciation 3 Excessive Descent PULL UP Pull Up A Rate Warning EDR Reduced Required PULL UP Terrain Terrain Pull Up gt Terrain Clearance or Pull Up ES Warning RTC or 2 Terrain Ahead Pull Up Terrain Ahead Pull Up TERRAIN AHEAD PULL UP Terrain Ahead Pull Up Ter T o eo E oO v Jeuonippy Imminent Terrain PULL UP Impact Warning ITI or rain Ahead Pull Up se Terrain Terrain Pull Up Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Obstacle Clearance or Up Pull Up E MAROC i 3 Obstacle Ahead Pull Up Obstacle Ahead Pull Up xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 63 Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Features Appendix Index Annunciations amp Alerts A GARMIN PFD MFD MFD Aler
17. database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Airport Terrain database mismatch The PFDs and MFD have different airport terrain database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on NAV DB UPDATED Active navigation database updated System has updated the active navigation database from the standby navigation database TERRAIN DSP PFD1 PFD2 or MFD1 Terrain awareness display unavailable One of the terrain airport terrain or obstacle databases required for TAWS in the specified PFD or MFD is missing or invalid GMA 1347D MESSAGE ADVISORIES Message Comments GMAT FAIL GMAT is inoperative GMA2 FAIL GMA2 is inoperative The audio panel self test has detected a failure The audio panel is unavailable The system should be serviced GMA XTALK GMA crosstalk error has occurred An error has occurred in transferring data between the two GMAs The system should be serviced GMA1 CONFIG GMAT config error Config s
18. 164 feet below the prescribed altitude at the Final Approach Fix Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION A WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVS is intended as an aid to situational awareness only and may not provide the accuracy and or fidelity upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic A WARNING Do not use SVS runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing Synthetic Vision System SVS functionality is offered as an enhancement to the G1000 system SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots perspective SVS information is shown on the primary flight display PFD In addition to SVS enhancement to the PFD the following features have been added to the PFD e Pathways e Flight Path Marker e Horizon Heading Marks e Terrain and Obstacle Alerting e Three dimensional Traffic e Airport Signs e Runway Display Displaying SVS Terrain 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 Press the SYN TERR Softkey 4 Press t
19. 49 50 Airways 94 Alert messages 80 ALT 46 Altitude mode 46 Altitude volume 46 Antenna stabilization 44 Antenna tilt 42 AOPA Airport Directory 52 AP 62 Attitude amp Heading Reference System 62 Audio panel controls NAV1 NAV2 6 Barometric Altitude Minimums 3 Barometric pressure 91 Bearing line 42 43 C CDI 1 2 6 84 Cell 37 38 Cell mode 38 Channel Presets 54 ChartView 50 51 190 00664 02 Rev B Index Checklists 57 58 Code selection softkeys 5 COM 5 6 D DB Mismatch 95 Declutter 88 94 Direct to 13 DME 5 6 E Edit a flight plan 30 Electronic Checklists 57 58 Electronic Stability and Protection 55 Emergency Checklist 58 ESP 55 56 F FD 62 Flight Director 9 Flight path marker 49 FliteCharts 50 51 Frequency Transfer 6 G Gain 43 H HF 5 6 Horizon heading 49 Horizontal scan 42 Inhibit 47 Inhibit TAWS 47 Inset Map 87 88 IOI 64 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi_ Index 1 su jy unuuy sainjea4 aouepioay saunpar0ld Buruue d AEN Sd5 24V oipny udax sjueumnansu jeuonippy puezey qybil4 U10 AEN Wi x pu ddy Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Annun Alerts Appendix Index J Jeppesen 51 L Level Mode 55 Lightning 37 38 88 M Magnetic Field Variation Database 99 100 Map panning 39 Message advisories 67 86 MET 62 METAR 39 88
20. Buruue d AEN Sd5 24V oipny uddx sjueumnansu jeuonippy puezey qy6il4 U10 AEN Wi x pu ddy Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional AFCS GPS Nav Procedures Annun Alerts Features Appendix A Index GARMIN Blank Page Index 4 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 190 00664 02 Rev B A GARMIN Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A p 913 397 8200 f 913 397 8282 Garmin AT ana 2345 Turner Road SE Salem OR 97302 U S A p 503 391 3411 f 503 364 21 Garmin Europe Ltd Liberty House Bulls Copse Roa Hounsdown Business Park Southampton S040 9RB U K p 44 0870 8501241 f 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 www garmin com 2007 2009 2012 Garmin Ltd or its subsidiaries 190 00664 02 Rev B
21. COM input signal is detected during play of a recorded memory block play is halted Pressing the PLAY Key twice within one half second while audio is playing plays the previous block of recorded audio Each subsequent two presses of the PLAY Key within one half second backtracks through the recorded memory blocks to reach and play any recorded block 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 7 su jy unuuy sainjea4 eouepioAy SaJnpa20Jd Buruuejd AEN SdD S24V oipny YddX sjueumasu Jeuonippy paezey W0 gt AeN xipuaddy xopu 36114 34614 A Nav Com XPDR Audio Panel GARMIN Flight Instruments Nav Com zm Ei zi E 4 a a x lt GPS Nav AFCS Flight Planning Blank Page Additional Hazard Appendix Annun Alerts Features Avoidance Procedures Index 8 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 190 00664 02 Rev B GARMI N AES AUTOMATIC FLIGHT CONTROL SYSTEM A NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis syu un su 1i SE Z2 E DO eg ER o A NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key lis
22. COMPARATOR ANNUNCIATIONS Comparator Window Condition Text ACN Sd5 Difference in altitude sensors is gt 200 ft f both airspeed sensors detect 35 knots this is inhibited Buruue d 16114 f either airspeed sensor detects gt 35 knots and the difference in sensors is gt 10 kts f either airspeed sensor detects gt 80 knots and the difference in sensors is gt 7 kts HDGMISCOMP Difference in heading sensors is gt 6 degrees s Np IO0ld Difference in pitch sensors is gt 5 degrees ROLMISCOMP Difference in roll sensors is gt 6 degrees o data from one or both altitude sensors o data from one or both airspeed sensors o data from one or both heading sensors o data from one or both pitch sensors o data from one or both roll sensors aouepionay puezey SoJnjeoj Jeuonippy gt k o Fl a Ej xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 61 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index Annunciations amp Alerts REVERSIONARY SENSOR ANNUNCIATIONS A GARMIN Reversionary Sensor Window FDs are di Condition m ber one Air Data Computer FDs are di m ber two Air Data Computer FDs are di FDs are di m m ber one Attitude amp Headin
23. Copy a Flight Plan er etre tete Delete a Flight Plan tt tnr diete Graphical Flight Plan Creation sse Export a Flight Plan to an SD Card PROCEDURES niiina a Load and Activate a Departure Procedure ss Activate A Departure Leg Load An Arrival Procedure Activate An Arrival Leg Load and or Activate an Approach Procedure ssssssss Activate An Approach in the Active Flight Plan Activate a Vector to Final Approach Fix sss Activate A Missed Approach in the Active Flight Plan HAZARD AVOIDANCE e 37 ADDITIONAL FEATURES Customizing the Hazard Displays on the Navigation Map 37 STORMSCOPE Optional sssseeennennnnnnnnn SiriusXM Weather Optional Airborne Color Weather Radar 41 Traffic Systems sseeeeeeteentrttte nennt ttti ttti 44 Terrain Awareness amp Warning System TAWS Display ssss 46 Synthetic Vision Terminal Procedure Charts Airport Directory sssssssseeenennnnennnnennrnnnnnt nennen SiriusXM Satellite Radio Electronic Stability amp Protection ESP Electronic Checklists rec tct em cti Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMIN table of Contents ANNUNCIATIONS
24. Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The system should be serviced NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The system should be serviced 15 aoueploay seinpa2oJd Buruue d AEN Sd5 24V oipny uddx Sjueuinjjsu paezey Wij w09 eN 1014 SoJnjeeoj Jeuonippy di PEOR xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix mt Index Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message MANIFEST NAV1 software mismatch communication halted MANIFEST NAV2 software mismatch communication halted Comments NAV1 and or NAV2 software mismatch The system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck The r
25. Hawker Beechcraft C90A GT GTi 190 00664 02 Rev B GARMIN cs Navigation NOTE Making course changes greater than 90 during a descent with vertical guidance may cause excessive and rapid movement of the vertical deviation indicator and SVS Pathways The system updates vertical path guidance continuously using ground speed and the calculated distance to the Bottom of Descent BOD Due to turn anticipation guidance turn smoothing distance to the BOD can be affected by course changes greater than approximately 5 degrees Ground speed can be affected by factors such as shifts in wind direction aircraft power management pitch angle and course changes Abrupt and or substantial changes to either the distance to the BOD ground speed or both can cause similarly abrupt substantial changes in vertical path guidance Because of turn smoothing changes to both distance to the BOD and ground speed tend to be more extreme when the BOD is also a waypoint that marks a large course change These speed and distance changes will be accounted for in the computed required vertical path and reflected in the vertical guidance indications 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft COOA GT GTi 17 oipny uddx sjueumasu S2dV ge gt a sy jy unuuy soinjes a2ueploAy SeJnpa oJd Jeuonippy paezey xipuaddy x pul 36114 U10 AEN Eg Flight Instruments Nav Com XPDR Aud
26. Key 10 With LOAD highlighted press the ENT Key 11 The arrival will become part of the active flight plan ACTIVATE AN ARRIVAL LEG 1 2 3 4 5 Press the FPL Key on the Control Unit to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the arrival Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed With ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 34 1 2 3 4 5 6 NOTE If certain GPS parameters SBAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Press the ENT Key A list of available approaches for the destination airport is displayed Turn either FMS Knob to highlight the desired approach Press the ENT Key A list of available transitions for the selected approach procedure is now displayed Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARM
27. TMR REF Displays Timer References Window z NRST Displays Nearest Airports Window d ALERT Displays Alerts Window e MFD SOFTKEY MAP Fs F EF F V3 V3 V3 V T ks B SeJnpa oJd Select the BACK Softkey on this level to return to the top softkey level optional optional optional z TERR EE E me VF F amp A V3 FP PE SEU EE MFD Softkeys E 5 a a gt so o ri a E xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 93 Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Appendix Level 1 Level 2 A GARMIN Description MAP DCLTR 3 SHW CHRT CHKLIST TRAFFIC TOPO TERRAIN AIRWAYS STRMSCP NEXRAD XM LING METAR LEGEND BACK Enables second level Navigation Map softkeys Displays traffic information on Navigation Map Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map Displays terrain information on Navigation Map Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed Displays Stormscope weather and coverage information on Navigation Map optional feature Displays NEXRAD weather
28. 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 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 83 eouepioAy senpa2oJd Buruue d AEN Sd5 24V oipny uddx SjueuinJjsu paezey Wija w09 eN Wija sainjea4 Jeuonippy xipuaddy xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix MES Index Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message Comments DB CHANGE Database changed Verify stored airways This occurs when a stored flight plan contains an airway that is no longer consistent with the 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 LOCKED FPL Cannot navigate locked flight plan This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at waypoint 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 air
29. and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts FliteCharts resemble the paper version of AeroNav Services terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 Select the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and select the SHW CHRT Softkey 2 Select the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Note that NOTAMS are only available with ChartView 3 Select the GO BACK Softkey to return to the previous page 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 5 Sa1npa20Jg Buruue d AEN Sd5 S 041V oipny uddx sjueumasu fila u105 NeN fila aouepioay puezey xipuaddy su jy unuuy EE Jeuonippy xepu Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun A
30. and press the ENT Key Repeat step numbers 4 and 5 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN Flight Planning IMPORT A FLIGHT PLAN FROM AN SD CARD sjuaumasu fi 1 Insert the SD card containing the flight plan in the top card slot on the MFD 2 Press the FPL Key on the Control Unit to display the Active Flight Plan Page EE on the MFD ES 3 Turn the small FMS Knob to select the Flight Plan Catalog Page 4 Press the FMS Knob to activate the cursor 5 Turn either FMS Knob to highlight an empty or existing flight plan 6 Select the IMPORT Softkey If an empty flight plan is selected a list of the available flight plans on the SD card will be displayed Or If an existing flight plan is selected an Overwrite existing flight plan OK or CANCEL prompt is displayed Press the ENT Key to choose to overwrite the selected flight plan and see a list of the available flight plans on the SD card If overwriting the existing flight plan is not desired select CANCEL using the FMS Knob press the ENT Key select another existing or empty flight plan and again select the IMPORT Softkey 7 Turn the small FMS Knob to highlight the desired flight plan for importing 8 Press
31. audio configuration The system should be serviced GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature The GIA1 and or GIA2 temperature is too high If problem persists the system should be serviced GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The system should be serviced 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 13 eouepioAy seinpa2o0Jd Buruue d AEN Sd5 241V oipny uddx SjueuinJjsu paezey Wij w09 eN Wijd SoJnjeoj Jeuonippy S ical xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix MEA Index Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message Comments HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted A GIA mismatch has been detected where only one is SBAS capable MANIFEST GIA1 software mismatch communication
32. be active when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the departure 4 Select the ACT LEG Softkey A confirmation window showing the selected leg will be displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 4 Turn the large FMS Knob to highlight the desired arrival 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi Procedures 33 AEN SdD S24V oipny uadx sjueumasuj u105 NeN fila Buruuejd 36114 So1Jnpa oJd su jy unuuy sainjea4 aouepioay jeuonippy paezey xipuaddy xopu Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Procedures GARMI N 5 6 1 8 9 Press the ENT Key A list of transitions is displayed for the selected arrival Turn either FMS Knob to select the desired transition Press the ENT Key A list of runways is displayed for the selected arrival Turn the large FMS Knob to highlight the desired runway Press the ENT
33. between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Enable Disable Aviation Data 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key TAWS Inhibit Inhibit TAWS While the TAWS B Page is displayed select the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit TAWS 3 Press the ENT Key 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi Hazard Avoidance 4 AEN SdD S24V oipny uadx sjuoumnasuj u105 NeN fila Buruuejd 34614 ERIT SaJnpa oJd puezey sainjea4 jeuonippy su jy unuuy x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Additional AFCS GPS Nav Procedures v v 5 aS E lt x Appendix Annun Alerts Features Index Hazard Avoidance GARMI N Enable TAWS While the TAWS B Page is displayed select the INHIBIT Softkey Or 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable TAWS 3 Press the ENT Key A NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active 48 waypoint in a GPS SBAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least
34. card exported Flight plan export failed The stored flight plan was not successfully exported to the SD card The SD card may not have sufficient available memory or the card may have been removed prematurely 66 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES Message DATA LOST Pilot stored data was lost Recheck settings Comments The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings if desired XTALK ERROR A flight display crosstalk error has occurred The MFD and PFDs are not communicating with each other The system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair PFD2 SERVICE PFD2 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair The PFD and or MFD self test has detected a problem The system should be serviced MANIFEST PFD1 software mismatch communication halted MANIFEST PFD2 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The system should be serviced PFD1 CONFIG PFD1 config error Config service req d PFD2 CONFIG P
35. cursor over the ALT altitude field 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 13 oipny uddx syueumasu U10 AEN S2dV su jy unuuy sainjea4 aouepioay Sa1npa oJd Buruue d jeuonippy paezey xipuaddy xopu fila 3464 Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index GPS Navigation GARMI N 1 8 9 10 11 12 13 14 15 Turn the small FMS Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET offset distance field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key on the Control Unit and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to ac
36. eack aens nps amp mnmnnmnunn NA CEE eerers jJ w j we Teck F3 V3 V3 P3 A ng nmn mnm w cm cme omms oc JDL Lec J ters A ES A V3 9F amp 75n5 nn onm w En erR hezea fersen LL dE ssec J ates F3 P3 rs m s nono on 5 n n PFD Configuration Softkeys Level 1 Level2 Level 3 Description PFD Displays second level softkeys for additional PFD configurations SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction HRZN HDG Displays compass heading along the Zero Pitch line APTSIGNS Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm 90 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN 1 1 Appendix Level 1 Level 2 Level 3 Description B DFLTS Resets PFD to default settings including s changing units to standard WIND Displays softkeys to select wind data Sz ER parameters P OPTN 1 Direction arrow and numeric speed E OPTN 2 Direction arrow with numeric direction S2dV and magnitude OPTN 3 Headwind tailwind and crosswind arrows with numeric speed components OFF Information not displa
37. grants permission to down other oad a single copy of this manual and of any revision to this manual onto a hard drive or electronic storage medium to be viewed for personal use provided that such electronic 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 Garmi n G10009 WATCH FliteCharts and SafeTaxi are registered trademarks of Garmin Ltd or its subsidiaries ESP is a trademark of Garmin Ltd or its subsidiaries These trademarks may n of L 3 ot be used without the express permission of Garmin NavData is a registered trademark of Jeppesen Inc Stormscope is a registered trademark Communications SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio Inc AOPA Membership Publications Inc and it AOPA expressl data express or imp and fitness for a warrant or make no circumstan consequential possibility of s by itation or exc the above lim AC U KWIK and expressly disclai in this data exp merchantabili AC U K eliabilit maximum extent from any cause o lim so do not allow the consequential damages so the above limitations or exclusions may not apply to lice November 2012 ces in dama do
38. halted MANIFEST GIA2 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The system should be serviced MANIFEST GFC software mismatch communication halted Incorrect servo software is installed or gain settings are incorrect MANIFEST COM1 software MANIFEST COM 2 software mismatch communication halted mismatch communication halted COM1 and or COM2 software mismatch The system should be serviced Reducing transmitter power COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM2 over temp The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the system should be serviced COM1 SERVICE COM1 needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may still be usable The system should be serviced when possible COM1 PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The COM1 and or COM2 external push to talk Switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the system should be serviced with other NAVS LOI GPS integrity lost Crosscheck
39. in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD and or PFDs detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Airport Directory database error exists The MFD detected a failure in the Airport Directory database Ensure that the data card is properly inserted Replace data card If problem persists the system should be services 70 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 190 00664 02 Rev B A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 multiple database error exists PFD1 DB ERR PFD1 multiple database error exists PFD2 DB ERR PFD2 multiple database error exists Comments The MFD and or PFD detected a failure in more than one database If problem persists the system should be serviced DB MISMATCH Navigation database mismatch Xtalk is off The PFDs and MFD have different navigation database versions or regions installed Crossfill is off Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Pa
40. information The 1 AHRS is not receiving backup GPS information The system should be serviced AHRS2 GPS AHRS2 not receiving backup GPS information The 2 AHRS is not receiving backup GPS information The system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The system should be serviced AHRS2 GPS AHRS2 operating exclusively in no GPS mode The 2 AHRS is operating exclusively in no GPS mode The system should be serviced 78 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 190 00664 02 Rev B A GARMIN Annunciations amp Alerts GRS 77 MESSAGE ADVISORIES CONT Message AHRS MAG DB AHRS magnetic model database version mismatch Comments The 1 AHRS and 2 AHRS magnetic model database versions do not match AHRS1 SRVC AHRS1 Magnetic field model needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical AHRS2 SRVC AHRS2 Magnetic field model needs update The 2 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far North South no magnetic compass GEO LIMITS AHRS2 too far North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as i
41. initiated self Passed test optional E Skywatch System Test Played when the optional SKY497 TAS system fails a pilot initiated self test Failed optional xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 65 Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts A GARMIN FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Results Flight plan successfully imported File contained user waypoints only User waypoints imported successfully No stored flight plan data was modified Description A flight plan file stored on the SD card was successfully imported as a stored flight plan The file stored on the SD card did not contain a flight plan only user waypoints These waypoints have been saved to the system user waypoints No flight plans stored in the system have been modified 0 flight plan files found to import The SD card contains no flight plan data Flight plan import failed Flight plan data was not successfully imported from the SD card Flight plan partially im ported Some flight plan waypoints were successfully imported from the SD card however others had errors and were not imported A part
42. on the MFD 2 Select the RA TEST Softkey RA TEST is displayed to the left of the Radar Altitude window The Radar Altitude window displays 50 feet indicating a properly functioning system soinjeo Jeuonippy 3 Selecting the RA TEST Softkey again or exiting the System Status Page cancels the test su jy unuuy DISPLAYING WIND DATA xipuaddy 1 Press the PFD Softkey 2 Press the WIND Softkey to display wind data below the Selected Heading 3 Press one of the OPTN softkeys to change how wind data is displayed 4 Toremove the Wind Data Window press the OFF Softkey xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 3 Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional AFCS GPS Nav Procedures Appendix Annun Alerts Features Index Flight Instruments Blank Page 4 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi A GARMIN 190 00664 02 Rev B A GARMIN __ Makom KERRANG Panel NAV COM TRANSPONDER AUDIO PANEL ADF TUNING OPTIONAL Tune the ADF using the remote ADF control head DME TUNING 1 2 3 4 Press the DME Softkey Turn the large FMS to select the DME source field Turn the small FMS Knob to select the desired Nav radio Press the ENT Key to complete the selection ENTER A TRANSPONDER CODE 1 2 3 4 Press the XPDR Softkey to display the transponder
43. section If the self test fails the system will revert to Standby Mode and a voice alert appropriate for the installed system will be heard indicating the test failed 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi AEN SdD S24V oipny uadx sjuoumnasuj u105 AeN 36114 Buruue d 16114 ERIT saunpa20ld puezey sainjea4 jeuonippy su jy unuuy xipuaddy xopu Flight Instruments Nav Com XPDR Audio Flight Planning Additional AFCS GPS Nav Hazard Avoidance Procedures Appendix Annun Alerts Features Index Hazard Avoidance A GARMIN Displaying Traffic on the Traffic Map Page 1 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the second rectangular page icon Select the NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select the ALT MODE Softkey to change the altitude display volume Select the desired altitude volume by selecting the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field Select the STANDBY Softkey to place the system in the Standby Mode STANDBY will be displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Displaying Traffic on the Navigation Map 1 2
44. slot of each PFD and the MFD 3 Turn the system ON A prompt is displayed DO YOU WANT TO UPDATE THE STANDBY NAVIGATION DATABASE ON THE BOTTOM CARD THE STANDBY DATABASE WILL BE ACTIVATED UPON THE FIRST ON GROUND POWER CYCLE ON OR AFTER 00 00 SYSTEM TIME ON THE EFFECTIVE DATE TO FROM REGION WORLDWIDE WORLDWIDE CYCLE 1284 12805 EFFECTIVE 9 APR 2012 7 MAY 2012 EXPIRES 7 MAY 2812 84 JUN 2812 NO WILL BE ASSUMED IN 21 SECONDS 4 Press the YES Softkey The navigation database is copied to the SD card in the bottom card slot of the MFD 5 After the navigation database files are copied to the bottom SD card press any key to continue as instructed 7 Again press any key to continue as instructed on the display 8 Press the NO Softkey The display now starts in normal mode Since the database effective date is not yet valid it should not be loaded as the active database The display now starts in normal mode Do not remove power while the display is starting 9 Press the ENT Key to acknowledge the startup screen 10 Turn the large FMS Knob to select the AUX Page group on the MFD 11 Turn the small FMS Knob to select the System Status Page 12 w D The new database is copied to the SD card in the bottom card slot of each PFD Progress can be monitored in the SYNC STATUS field When copying is finished Complete is displayed 13 Turn system power OFF 98 Garmin G1000 Cockpit Reference Guide f
45. the ENT Key S2dV AEN Sd5 R e a o 2 S E 1 v aouepioay puezey INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN soinjes Jeuonippy 1 Press the FPL Key on the Control Unit to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint will be inserted before the highlighted waypoint su jy unuuy 4 Turn the small FMS Knob The Waypoint Information Window is now displayed xipuaddy 5 Enter the new flight plan waypoint by one of the following a Enter the user waypoint identifier facility or city b Press the ENT Key Or xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 2 Flight Instruments Nav Com XPDR Audio Hazard Additional AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning A GARMIN a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airport waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints
46. to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be deleted 5 Select the DELETE Softkey A Delete flight plan amp confirmation window is displayed 6 With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key on the Control Unit to display the Active Flight Plan Page 2 Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan AEN Sd5 zn gt EI Eh ti Ssye y unuuy SoJnjeeo4j 9 uepioAy SoJnpa oJd Jeuonippy paezey xipuaddy xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 31 Flight Instruments Nav Com XPDR Audio Hazard Additional AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning 3 4 5 A GARMIN The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion point Select the LD WPT Softkey The selected waypoint will be inserted at the selected point The d
47. 2 13 14 xipuaddy xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 23 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning A GARMIN CREATE A USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM 24 1 2 3 4 5 6 1 8 9 10 ANOTHER WAYPOINT Turn the large FMS Knob on the MFD Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD DIS radial distance Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field
48. 69 CONFIG GDL 69 config error Config service req d Comments GDL 69 configuration settings do not match those of backup configuration memory The system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The system should be serviced MANIFEST GDL software mismatch communication halted The GDL 69 has incorrect software installed The system should be serviced GWX 68 ALERT MESSAGES Message Comments GWX CONFIG GWX config error Config service req d GWX 68 configuration settings do not match those of the GDU configuration The system should be serviced GWX FAIL GWX is inoperative The GDU is not recieving 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 A failure has been detected in the GWX 68 The GWX 68 may still be usable MANIFEST GWX software mismatch communication halted The GWX 68 has incorrect software installed The system should be serviced WX ALERT Possible severe weather ahead 80 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm 190 00664 02 Rev B A GARMIN GDC 74B MESSAGE ADVISORIES Annuncia
49. 94 Minimums 65 MISCOMP 61 Mistrim 62 63 Mode S 92 Mode selection softkeys 5 Multi Function Display MFD Softkeys 93 MV DB 99 N NAV 2 6 Navigation database 15 16 NEXRAD 39 88 94 0 OBS 2 Obstacles 72 74 P Pathways 49 50 PIT 61 Power up Page 57 Index 2 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi A GARMIN R ROC 63 64 S SafeTaxi 50 SBAS 10 34 48 74 75 Sector scan 43 Secure Digital SD card 57 Sensor 62 STAB 44 Standby 41 Standby Navigation Database 98 Store Flight Plan 29 Stormscope lightning data 37 38 88 Strike 37 Strike mode 38 SVS 49 86 SVS Terrain 49 Synchronization 95 SYNC Status 98 Synthetic Vision System 49 T TA 65 TAF 39 TAS 45 46 78 TAWS 46 47 48 63 65 TAWS B 46 Terrain 46 71 88 94 Tilt line 42 Timer 83 Topographical data 88 94 Traffic 37 45 94 Traffic Advisory 45 65 Traffic map page 45 46 Transponder 5 92 93 190 00664 02 Rev B A GARMIN V Vertical speed guidance 16 Vertical track 65 VNV 13 85 Vspeed 2 W WATCH 44 Waypoint Selection Submenu 26 Weather Attenuated Color Highlight 44 Weather data link page 39 Weather radar 41 Wind data 91 X XM lightning 88 94 XM Radio 53 54 XM weather 39 XPDR Softkey 5 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi Index 3 Index su jy unuuy sainjea4 aouepioay saunpar0ld
50. A NAV RADIO 1 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VOR1 LOC1 NAV1 or VOR2 LOC2 NAV2 2 Press the NAV1 NAV2 DME or ADF Key on the audio panel to select or deselect the navigation radio audio source All radio keys can be selected individually or together NAV COM TUNING 1 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned N Turn the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz 3 Press the Frequency Transfer Key to place the frequency into the active frequency field INTERCOM Pressing the INTR COM Key on either Audio Panel selects and deselects the intercom on both Audio Panels The annunciator is lit when the intercom is active The intercom connects the pilot and copilot together Either the pilot or copilot may select or deselect the intercom The CABIN Key initiates two way communication between the pilot or copilot and the passengers in the cabin The annunciator is lit when the cabin intercom is active on either Audio Panel The MAN SQ Key allows either automatic or manual control of the intercom squelch setting Pressing the MAN SQ Key enables manual squelch control indicated by the MAN SQ annunciator During manual squelch operation pressing the ICS Knob switches between volume an
51. EN Sd5 89 APR 2812 7 MAY 2612 7 MAY 2812 84 JUN 2612 Buruue d 1614 NO WILL BE ASSUMED IN 8 SECONDS 5 After the update completes the display starts in normal mode SeJnpa o0Jd 6 Turn the system OFF and remove the SD card from the top card slot 7 Repeat steps 1 through 6 for the other displays PFD1 PFD2 or MFD 8 Apply power to the system and press the ENT Key to acknowledge the startup Screen 9 Turn the large FMS Knob to select the AUX Page group on the MFD aouepioay puezey 10 Turn the small FMS Knob to select the System Status Page ee 11 Press the Display Database Selection Softkey to show active navigation a3 database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct active navigation database cycle information is shown for each E display gt so o ri a E xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 97 Additional Hazard Flight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index A Appendix GARMIN Loading the Standby Navigation Database NOTE After the navigation database is loaded or copied the top SD card may be removed 1 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD 2 Verify that an SD card is inserted in the bottom
52. FD2 config error Config service req d The PFD configuration settings do not match backup configuration memory The system should be serviced MFD1 CONFIG MFD1 config error Config service req d SW MISMATCH GDU software version mismatch Xtalk is off The MFD configuration settings do not match backup configuration memory The system should be serviced The MFD and PFDs have different software versions installed The system should be serviced 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 67 aoueploay seinpa2oJd Buruue d AEN Sd5 24V oipny uddx Syueuingjsu paezey Wija U405 AEN Wi SoJnjeoj Jeuonippy Ek acted xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts A GARMIN MFD amp PFD MESSAGE ADVISORIES CONT Message PFD1 COOLING PFD1 has poor cooling Reducing power usage PFD2 COOLING PFD2 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage Comments The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the system should be serviced PFD1 KEYSTK PFD1 key name Key is stuck PFD2 KEYSTK PFD2 key name Key is stuck MFD1 KEYSTK MFD key name
53. FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key The active flight plan is modified as each waypoint is entered Repeat step numbers 3 and 4 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to remove the cursor Creating a stored flight plan 1 2 3 4 5 6 7 Press the FPL Key Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page Select the NEW Softkey or press the MENU Key highlight Create New Flight Plan and press the ENT Key to display a blank flight plan for the first empty storage location Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints
54. G1000 Integrated Flight Deck Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi Y GARMIN Copyr This m Beech ight 2007 2009 2012 Garmin Ltd or its subsidiaries All rights reserved anual reflects the operation of System Software version 0636 03 or later for the Hawker craft COQA GT GTi Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions Garmi n International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmi n AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmi n Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton S040 ORB U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garmi n Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 STI Web Site Address www garmin com Except or after hours emergency aircraft on ground AOG technical support for Garmin panel mount and integrated avionics systems please contact Garmin s AOG Hotline at 913 397 0836 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
55. IN 7 8 9 10 11 w wo Press the ENT Key The cursor moves to the MINIMUMS field If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected approach procedure Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and is immediately activated 12 Press the ENT Key ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL Press the ENT Key The final approach course becomes the active leg ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH Press the ENT Key A confirmation
56. Instruments GARMIN CHANGE NAVIGATION SOURCES 1 2 3 Press the CDI Softkey to change from GPS to VOR1 or LOC1 This changes the NAV1 standby frequency in the upper left corner of the PFD to light blue indicating this is the frequency selected for tuning Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This changes the NAV2 standby frequency in the upper left corner of the PFD to light blue indicating this is the frequency selected for tuning Press the CDI Softkey a third time to return to GPS ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 Press the OBS Softkey to select OBS Mode 2 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 3 Press the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 Press the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted 2 Turn the small FMS Knob to display the UP DOWN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted 3 Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it will start counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window CONFIGURE VSPEED BUGS INDIVIDUA
57. Key Once all changes have been made press the FMS Knob to remove the cursor INVERT AND ACTIVATE A STORED FLIGHT PLAN 30 1 2 3 Press the FPL Key on the Control Unit Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMIN Flight Planning 4 Turn the large FMS Knob to highlight the desired flight plan 5 Select the INVERT Softkey Invert and activate stored flight plan will be displayed 6 With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location sjueuinisu 1i oipny uddx UI05 AEN COPY A FLIGHT PLAN S2dV 1 Press the FPL Key on the Control Unit 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be copied 5 Select the COPY Softkey A Copy to flight plan confirmation window is displayed 6 With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN 1 Press the FPL Key on the Control Unit 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob
58. LLY 1 2 3 4 Press the TMR REF Softkey Turn the large FMS Knob to highlight the desired Vspeed Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to the speed Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMIN Flight instruments 5 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 6 To remove the window press the CLR Key or the TMR REF Softkey EL a ga c ERG o gt 3 FA a TURN VSPEED BUGS ON OR OFF BY CATEGORY oipny uddx U105 AEN 1 Press the TMR REF Softkey 2 Press the MENU Key 3 Turn the FMS Knob to highlight the desired option 4 Press the ENT Key Press the TMR REF Softkey to remove the window S2dV SET BAROMETRIC RADAR ALTIMETER MINIMUM DESCENT ALTITUDE AEN Sd5 1 Press the TMR REF Softkey 2 Turn the large FMS Knob to highlight the OFF BARO RAD ALT field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to select BARO or RAD ALT 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 Toremove the window press the CLR Key or the TMR REF Softkey seinpa2o0Jd Buruue d 1614 aouepioay puezey TESTING THE RADAR ALTIMETER 1 Select the AUX SYSTEM STATUS Page
59. Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 2 1 2 Press the MENU Key with the Navigation Map Page displayed Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page Turn the large FMS Knob until the Map Page group is selected Turn the small FMS Knob select the Stormscope Page Change the Stormscope Lightning Mode Between Cell and Strike 1 2 Select the Stormscope Page Select the MODE Softkey The CELL and STRIKE Softkeys are displayed Select the CELL Softkey to display CELL data or select the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the Viewing Mode Between 360 and 120 1 2 Select the Stormscope Page Select the VIEW Softkey The 360 and ARC Softkeys are displayed Select the 360 Softkey to display a 360 viewing area or select the ARC Softkey to display a 120 viewing area Select the CLEAR Softkey to remove all Stor
60. NOTE Do not rely solely upon data link services to provide Temporary Flight Restriction TFR information Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN Index 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 NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features o
61. T Flight Instruments System Annunciation Comment Nav Com XPDR Audio Display system is not receiving airspeed input from air data computer AFCS Display system is not receiving altitude input from the air data computer GPS Nav Flight Planning Display system is not receiving vertical speed input from the air data computer Procedures Hazard Avoidance A red X through any other display field such as engine instrumentation display indicates that the field is not receiving valid data Other Various Red X Indications Bu E Eej sr X ADVISORY ANNUNCIATIONS Annunciation Alerts Window Text Window Text AVN FAN 1 FAIL Avionics cooling fan 1 is inoperative AVN FAN 2 FAIL Avionics cooling fan 2 is inoperative PFD 1 FAN FAIL PFD 1 cooling fan is inoperative PFD 2 FAN FAIL PFD 2 cooling fan is inoperative MFD FAN FAIL MFD cooling fan is inoperative Appendix Index 60 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMIN Amunciations amp Alerts MESSAGE ADVISORY ALERTS Alerts Window Message ESP DEGRADE ESP IAS mode is inoperative ESP FAIL ESP is inoperative ESP OFF ESP selected off ESP CONFIG ESP config error Config service req d Available with ESP option only s u un su 1i oipny uddx U105 AEN S2dV
62. TS 22 1 2 3 4 5 6 7 8 9 10 Turn the large FMS Knob on the Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD RAD radial radial Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMIN Flight Planning a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints sjueuinisu 1i b Turn the large FMS Knob
63. a force to the appropriate control surface to return the aircraft to the desired flight envelope This is perceived by the pilot as resistance to control movement in the undesired direction when the aircraft approaches a steep attitude or high airspeed As the aircraft deviates further from the desired attitude or airspeed continues to increase the force increases up to an established maximum to encourage control movement in the direction necessary to return to the desired attitude and or airspeed range Except in the case of high airspeed when maximum force is reached force remains constant up to the maximum engagement limit Above the maximum engagement limit forces are no longer applied There is no maximum engagement related to a high airspeed condition When ESP has been engaged for more than ten seconds cumulative not necessarily consecutive seconds of a 20 second interval the autopilot is automatically engaged with the flight director in Level Mode in the pitch and roll axis bringing the aircraft into level flight An aural Engaging Autopilot alert is played and the flight director mode annunciation will indicate TVE for vertical and lateral modes The pilot can interrupt ESP by pressing and holding either the Control Wheel Steering CWS or Autopilot Disconnect AP YD DISC TRIM INTRPT switch Upon releasing the CWS or AP YD DISC TRIM INTRPT switch ESP force will again be applied provided aircraft attitude and or airspeed are wi
64. access the first five preset channels PS1 PS5 Select the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Pressing the MORE Softkey repeatedly cycles through the preset channels Select any one of the PS1 PS15 softkeys to assign a number to the active channel Select the SET Softkey on the desired channel number to save the channel as a preset Adjusting Volume 1 2 3 With the XM Radio Page displayed press the VOL Softkey Press the VOL Softkey to reduce volume or press the VOL Softkey to increase volume Once the VOL Softkey is pressed the volume can also be adjusted using the small FMS Knob Press the MUTE Softkey to mute the audio Press the MUTE Softkey again to unmute the audio Radio volume may also be adjusted at each passenger station 54 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B amp GARMIN Additional Features ELECTRONIC STABILITY amp PROTECTION ESP A NOTE Refer to the Airplane Flight Manual to determine approval of ESP functionality The optional Garmin Electronic Stability and Protection ESP system is available only when the GFC 700 AFCS is installed ESP engages when the aircraft exceeds one or more conditions pitch roll Vmo and or Mmo beyond the normal flight param eters Enhanced stability for each condition is provided by applying
65. and coverage information on Navigation Map optional feature Displays XM lightning information on Navigation Map optional feature Displays METAR flags on airport symbols shown on the Navigation Map optional Displays the legend for the selected weather products Available only when NEXRAD XM LTNG and or METAR softkeys are selected Returns to top level softkeys Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan When available displays optional airport and terminal procedure charts When available displays optional checklists 94 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN Appendix LOADING UPDATED DATABASES Ay CAUTION Never disconnect power to the system when loading a database Power interruption during the database loading process could result in main tenance being required to reboot the system A NOTE When loading database updates the DB Mismatch message will be displayed until database synchronization is complete followed by turning system power off then on Synchronization can be monitored on the AUX SYSTEM STATUS Page In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product f
66. ayed when pressing the ENT Key the next checklist in the group will be displayed If EXIT CHECKLISTS is displayed when pressing the ENT Key the system will exit the Checklist Page Select the EXIT Softkey to exit the Checklist Page and return to the page last viewed When returning to the Checklist Page after selecting the EXIT Softkey the system will return to the last select checklist item Immediately Accessing Emergency Procedures 1 2 3 4 5 6 7 8 From any page on the MFD select the CHKLIST Softkey or turn the large FMS Knob to select the Checklist Page Select the EMERGCY Softkey Turn the FMS Knob to select the desired emergency checklist and press the ENT Key Press the ENT Key or select the CHECK Softkey to check the selected emergency checklist item The line item turns green and a checkmark is placed in the box next to it The next line item is automatically highlighted for checking Either FMS Knob can be used to scroll through the checklist and select the desired checklist item Press the CLR Key or select the UNCHECK Softkey to remove a check mark from an item When all checklist items have been checked Checklist Finished is displayed in green text at the bottom left of the checklist window and GO TO NEXT CHECKLIST is highlighted If GO TO NEXT CHECKLIST is selected prior to checking all the checklist items CHECKLIST NOT FINISHED will be displayed in yellow tex
67. craft 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 APR INACTV Approach is not active Special use airspace is within 2 nm of the aircraft position The system notifies the pilot that the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver 84 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 190 00664 02 Rev B A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message PTK FAIL Parallel track unavailable bad geometry Comments 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 pas
68. cumentation even if AOPA uch damages U aw to release and hold harmless AOPA fro its re m all warranti ess 0 ty and fit information arisin sclaim all ied inclu y di pa an ges that to any actual or alleged inaccuracies in the in usion it of impl atio ated or implie wise Licen allowed by f action clai g out of Ga imitation or ticular pu y representation duding n ns or exclusions may not ness for a particular pu WIK Organizations do not warrant or ma y or othe warranties with ding but not lim rpose The infor s regardin egligence sha esult from the or an AOPA aut Ser agrees not to AOPA be li use or inabi horized repr f orm iabi app f ied warranties o ganizations hereafter collecti es with respect d including but not pose The in e any rep see agrees not to s aw to release and hold harm ms or losses related to any ac rmin s use of the information exclusion of implied warranti 190 00664 02 Rev B S related organizations herei espect to the AOPA informati ted to the implied warranties mation is provided as is and AOPA does not g its accuracy reliability or sue AOPA and to the maximum m any causes of action claims or losses re ation Some jurisdictions do not allow the lity for incidental or consequential dam y to you ue AC U K f na on of merchanta oth able for any inc lit
69. cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 14 Press the ENT Key 15 Press the FMS Knob to remove the flashing cursor sodv AEN Sd5 11 R e a D 2 E o v aouepioay puezey DELETE A USER WAYPOINT soinjes Jeuonippy 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 4 Turnthe large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn the small FMS Knob to highlight the desired waypoint 6 Select the DELETE Softkey 7 Themessage Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key su jy unuuy x pu ddy x pul 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 25 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning A GARMIN CREATE A FLIGHT PLAN 26 NOTE When creating a flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Creating an active flight plan 1 2 3 4 5 6 Press the FPL Key Press the FMS Knob to activate the cursor only on MFD Turn the small
70. d in on the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing Selecting the DCLTR Softkey cycles through the different declutter levels DCLTR shows all map detail DCLTR 1 removes taxiway markings and airport identification labels DCLTR 2 removes VOR station ID the VOR symbol and intersection names 50 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMIN Additional Features if within the airport plan view DCLTR 3 removes the airport runway layout unless the airport in view is part of an active flight plan The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways ramps runways terminals and services This information should not be used by the pilot as the basis for maneuvering the aircraft on the ground This database is updated on a 56 day cycle ChartView ChartView resembles the paper version of Jeppesen terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts
71. d squelch adjustment lighting the associated annunciator beneath the knob When the MAN SQ annunciator is lit the ICS Knob controls both volume and squelch When the MAN SQ annunciator is extinguished the ICS Knob controls only volume 6 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN _ _ Makom APUR ANdio Panel PASSENGER ADDRESS PA SYSTEM A passenger address system is provided by pressing the PA Key to deliver messages to the passengers The message is heard by the other pilot on the headset only if the PA Key is enabled on both audio panels PA messages are one way from the flight deck to the passengers CLEARANCE RECORDER AND PLAYER NOTE Pressing the play key on the pilot s Audio Panel plays recorded audio to the Pilot Pressing the play key on the Copilot s Audio Panel plays recorded audio to the Copilot Recorded COM audio is stored in separate memory blocks Once 2 5 minutes of recording time have been reached the recorder begins recording over the stored memory blocks starting from the oldest block The PLAY Key controls the play function The PLAY annunciator is illuminated to indicate when play is in progress The PLAY annunciator extinguishes after playback is finished Pressing the PLAY Key once plays the latest recorded memory block and then returns to normal operation Pressing the PLAY Key again during play of a memory block stops play Ifa
72. e basic operation prior to actual use During flight operations carefully compare indications from the G1000 to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation WARNING 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 disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi amp Warnings Cautions amp Notes GARMIN WARNING Because of variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W
73. e small FMS Knob 3 Press the ENT Key Select an Available Channel within the Selected Category 1 While on the XM Radio Page select the CHNL Softkey 2 Select the CH Softkey to go up through the list in the Channel Box or move down the list with the CH Softkey Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels 3 With the desired channel highlighted press the ENT Key 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 53 SaJnpa oJd Buruue d AEN Sd5 24V oipny uddx sjueumnansu 16114 swop AeNn Wila aouepioay puezey xipuaddy su jy unuuy EE Jeuonippy xopu Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features GARMIN Entering a Channel Directly 1 2 3 4 While on the XM Radio Page select the CHNL Softkey Select the DIR CH Softkey The channel number in the Active Channel Box is highlighted Select the numbered softkeys located on the bottom of the display to directly select the desired channel number Press the ENT Key to activate the selected channel Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 2 3 4 On the XM Radio Page with the desired channel active select the PRESETS Softkey to
74. efault user waypoint naming is USROOO USROO1 USROO2 and so on To change the user waypoint name follow the procedure for modifying a user waypoint EXPORT A FLIGHT PLAN TO AN SD CARD 32 1 2 3 4 5 6 7 Insert the SD card into the top card slot on the MFD Press the FPL Key on the Contol Unit to display the Active Flight Plan Page on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be exported Select the EXPORT Softkey Press the ENT Key to confirm the export Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Turn the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure will
75. em should be serviced if the problem persists 190 00664 02 Rev B A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES Message FPL WPT LOCK Flight plan waypoint is locked Comments Upon power up the 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 This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved FPL TRUNC Flight plan has been truncated 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 This occurs when a newly installed navigation database eliminates an obsolete approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach TIMER EXPIRD Timer has expired The system notifies the pilot that the timer has expired DB CHANGE Database changed Verify user modified procedures This occurs when a stored flight plan contains procedures that have been manually edited
76. emote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cycle its operation If the problem persists the system should be serviced G S1 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The system should be serviced G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The system should be serviced when possible GEA 71 MESSAGE ADVISORIES Message GEA1 CONFIG GEAT config error Config service req d Comments The GEA1 configuration settings do not match those of backup configuration memory The system should be serviced GEA2 CONFIG GEA2 config error Config service req d The GEA2 configuration settings do not match those of backup configuration memory The system should be serviced MANIFEST GEA11 software mismatch communication halted The 1 GEA 71 has incorrect software installed The system should be serviced MANIFEST GEA2 software mismatch communication halted The 2 GEA 71 has incorrect software installed The system should be serviced 76 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraf
77. ervice req d GMA2 CONFIG GMA2 config error Config service req d 72 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi The audio panel configuration settings do not match backup configuration memory The system should be serviced 190 00664 02 Rev B A GARMIN Annunciations amp Alerts GMA 1347D MESSAGE ADVISORIES CONT Message MANIFEST GMAT software mismatch communication halted e Comments The audio panel has incorrect software installed The Service Return unit for repair MANIFEST GMA2 software System should be serviced mismatch communication halted GMA1 SERVICE GMAT needs The audio panel self test has detected a problem u GMA2 SERVICE GMA2 needs service Return unit for repair in the unit Certain audio functions may still be available and the audio panel may still be usable The system should be serviced when possible GIA 63W MESSAGE ADVISORIES Message Comments GIA1 CONFIG GIA1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d GIA1 CONFIG GIA1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d The GIA1 and or GIA2 configuration settings do not match backup configuration memory The system should be serviced The GIA1 and or GIA2 have an error in the
78. ess the ENT Key Vertically Scan a Storm Cell 1 While in the Horizontal Scan view move the Joystick to place the Bearing Line on the desired storm cell or other area to be vertically scanned 2 Select the VERTICAL Softkey A vertical slice of the selected area will now be displayed 3 Move the Joystick right or left to move the scanned slice a few degrees right or left 4 Turn the Joystick to adjust the range 5 To select a new area to be vertically scanned select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps 42 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMI amp IN ee Avoidance Adjusting Gain A WARNING Changing the gain in Weather Mode will cause precipitation intensity to be displayed as a color not representative of the true intensity Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation 1 Select th 2 Turn the small FMS Knob to adjust the gain for the desirable level The e GAIN Softkey to activate the cursor in the GAIN field gain setting is visible in the gain field as a movable horizontal bar in a flashing box The line pointer is a reference depicting the calibrated position 3 Press the FMS Knob to remove the cursor 4 Select the GAIN Softkey again to recalibrate the gain CALIBRATED will be dis
79. evisions GARMIN Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft COQA GT GTi 190 00664 02 Rev B GARMIN table of Contents FLIGHT INSTRUMENTS nnn 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg sss 1 Change Altimeter Barometric Pressure Setting Units sss 1 Synchronizing the Altimeter Barometric Pressure Settings 1 Synchronize CDI doe dee dete dee eite ed e de e deed Change Navigation Sources Enable Disable OBS Mode While Navigating with GPS sss 2 Generic Timer ne er eror nno REIR BUR BO NR RR UR E 2 Configure Vspeed Bugs Individually sss Turn Vspeed Bugs On or Off by Category Set Barometric Radar Altimeter Minimum Descent Altitude 3 Testing the Radar Altimeter ssssssseeeen ne 3 Displaying Wind Data 3 NAV COM TRANSPONDER AUDIO PANEL 5 ADF Tuning Optional sssseeenennnntnnnnnes 5 DIME Tanning enm eene t e a en o e a e s o e i 5 Enter a Transponder Code 5 Activate ADS B Transmit senes 5 Selecting a COM Radio 5 Selecting a NAV Radio 6 NAV COM Tuning sssseeeeennennnnnn nnns 6 Intercom deceat dae RA deo SU bom AU S deed 6 Passenger Address PA System 7 Clearance Recorder and Player 7 AUTOMATIC FLIGHT CONTROL SYSTEM
80. f the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the G1000 Pilot s Guide for this aircraft 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C9OA GT GTi RR 11 sainjea4 aouepioay saunpar0ld Buruue d AEN Sd5 24V oipny uddx syueumansu wio gt Aen Jeuonippy su jy unuuy gt 5 3 2 x 36114 164 puezey Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional AFCS GPS Nav Procedures Annun Alerts Features Appendix Index Blank Page A GARMIN RR 12 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft COOA GT GTi 190 00664 02 Rev B A GARMIN _______ Record of Revisions Change Summary 190 00664 00 Initial release at GDU 8 10 190 00664 01 Added Synthetic Vision System Added GDU 9 14 parameters 190 00664 02 Added GDU 12 05 parameters Added AC U KWIK Airport Directory references Added Electronic Checklist procedures Added METAR and weather LEGEND softkey functions Added Database update procedures Added MV DB update procedures Updated weather legend Updated SiriusXM references Updated message advisories Added VNAV NOTE Revision Date of Revision Affected Pages 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft COOA GT GTi RR 1 Record ofR
81. f the displayed data is shown at the right Not displayed when ECHO TOP is displayed 3m XM LIGHTNING The age of the displayed data is shown at the right 2m SIGMET 2m AIRMET 5m CELL MOVEMENT The age of the displayed data is shown at the right SIGMET amp AIRMET The age of the displayed data for each is shown at the right METAR Available for the US and Canada The age of the displayed data for each is shown at the right SURFACE ANALYSIS with CITY FORECAST The upper symbol depicts Surface Analysis The lower symbol depicts City Forecast The age of the displayed data for each is shown at the right The selected forecast period is shown at the bottom us 8m CN 12m 3000F1 FREEZING LEVEL The age of the displayed data is shown at the right WINDS ALOFT Available for the US and Canada The age of the displayed data for each is shown at the right The altitude selection is shown at the bottom COUNTY WARNING The age of the displayed data is shown at the right LDENEET CYCLONE WARNING The age of the displayed data is shown at the right m Aii AIREP The age of the displayed data is shown at the right 40 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 190 00664 02 Rev B A GARMIN Hazard Avoidance Wx Product Status Icons Description Oh 8m PIREP The age of the displayed data is shown at the right Urge
82. g Reference ber two Attitude amp Heading Reference FDs are di ber one GPS receiver FDs are di m ber two GPS receiver ir Data Computer 2 Air Data Computer HRS 2 AHRS 1 GPS 2 GPS AFCS ALERTS Condition Description Pitch Failure Pitch axis control failure Roll Failure Roll axis control failure Pitch Trim Axis If annunciated when AP is engaged a failure has occurred in Control Failure the pitch trim system Yaw Damper YD control failure Failure System Failure AP and MET are unavailable FD may still be available Elevator Mistrim A condition has developed causing the pitch servo to Up provide a sustained force in the nose up direction Elevator Mistrim CRE A condition has developed causing the pitch servo to Down provide a sustained force in the nose down direction 62 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMIN Amunciations amp Alerts Condition Annunciation Description Z Aileron Mistrim A condition has developed causing the roll servo to provide a gt Left ATL a sustained left force s Aileron Mistrim A condition has developed causing the roll servo to provide x Right AIL a sustained right force z E
83. ge for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Standby Navigation database mismatch The PFDs and MFD have different standby navigation database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Terrain database mismatch The PFDs and MFD have different terrain database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 71 eouepioAy seinpa2o0Jd Buruue d AEN Sd5 24V oipny uddx SjueuinJjsu paezey Wij U105 AEN Wija sainjea4 Jeuonippy xipuaddy xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Men Index Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Obstacle database mismatch Comments The PFDs and MFD have different obstacle
84. he BACK Softkey to return to the previous page 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 49 saunpa20ld Buruue d AEN Sd5 24V oipny udax sjueumnansu 16114 jwiop AeNn Wila aouepioay puezey xipuaddy su jy unuuy EE Jeuonippy xopu Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features GARMIN Displaying Pathways 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the PATHWAY Softkey 5 Press the BACK Softkey to return to the previous page Displaying Heading on the Horizon 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts it may be necessary to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjuste
85. he MENU Key to display the Page Menu 3 Turn the large FMS Knob to highlight Invert Flight Plan 4 Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location 5 With OK highlighted press the ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT PLAN oipny uddx syueumasu JU105 AEN Yid S2dV 1 Press the FPL Key on the Control Unit to display the active flight plan Press the FMS Knob to activate the cursor Or a Turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey 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 d e a o 2 m E oO v aouepioay puezey 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 soinjes Jeuonippy su jy unuuy 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 xipuaddy x
86. he traffic within range of the aircraft Due to lack of equipment poor signal reception and or inaccurate information from aircraft or ground stations traffic may be present that is not represented on the display WARNING Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information contained within data link weather products may not accurately depict current weather conditions WARNING Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product Due to time delays inherent in gathering and processing weather data for data link transmission the weather information shown by the data link weather product may be significantly older tha n the indicated weather product age 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 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 p
87. ial stored flight plan now exists in the system File contained user waypoints only The file stored on the SD card did not contain a flight plan only user waypoints One or more of these waypoints did not import successfully Too many points Flight plan truncated The flight plan on the SD card contains more waypoints than the System can support The flight plan was imported with as many waypoints as possible Some waypoints not loaded Waypoints locked The flight plan the system cannot find in the navigation database The been imported but must be edited within the system be activated for use on the SD card contains one or more waypoints that flight plan has ore it can be T3 User waypoint database full Not all loaded The flight plan file on the SD card contains user waypoints The quantity of stored user waypoints has exceeded system capacity therefore not all the user waypoints on the SD card have been imported Any flight plan user waypoints that were not imported are locked in the flight plan The flight plan must be edited within the System before it can be activated for use One or more user waypoints One or more imported user waypoints were renamed when imported renamed due to naming conflicts with waypoints already existing in the system Flight plan successfully The stored flight plan was successfully exported to the SD
88. iled operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 Press the MAP Softkey 2 Select the STRMSCP Softkey Select the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page Lightning Age Symbol Strike is less than 6 seconds old 4 Strike is between 6 and 60 seconds old Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old oe Select Cell or Strike as the Stormscope Lightning Mode 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight Map Setup 3 Press the ENT Key 4 Turn the small FMS Knob to highlight Weather 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 37 AEN SdD S24V oipny uadx sjuoumnasuj u105 NeN 36114 Buruue d 146114 ERIT saunpar0ld puezey sainjea4 jeuonippy su jy unuuy xipuaddy xopu Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Hazard Avoidance Procedures Additional Appendix Annun Alerts Features Index Hazard Avoidance 38 5 6 1 8 9 A GARMIN Press the ENT Key Turn the large FMS Knob to place the cursor in the STRMSCP MODE field Turn the small FMS Knob to display the Cell Strike window Turn either FMS Knob to select Cell or Strike Press the ENT Key Push the FMS Knob to return to the Navigation
89. ilot 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 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN Waminps Cautions amp Notes WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the G1000 Integrated Avionics System and GFC 700 AFCS in Hawker Beechcraft C90A GT GTi Airplane Flight Manual Supplement Thoroughly practic
90. io Flight Planning Hazard Avoidance Additional AFCS Procedures Appendix Annun Alerts Features Index GPS Navigation 18 Blank Page Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi A GARMIN 190 00664 02 Rev B GARMI N Flight Planning FLIGHT PLANNING sjueuinijsu 1i WEIGHT PLANNING All procedures apply to the MFD and the Control Unit unless otherwise stated oipny uddx U105 AEN Entering Weight Parameters The Weight Planning Page is displayed after system power up If it is necessary to return to this page turn the large FMS Knob to select the AUX page group Turn the small FMS Knob to select the Weight Planning Pge 1 Select the EMPTY WT Softkey to place the cursor in the Basic Empty Weight field 2 Enter the desired aircraft empty weight 3 Press the ENT Key The cursor is now over the PILOT amp STORES field 4 Enterthe desired weight of Pilot amp Stores 5 Press the ENT Key 6 Continue repeating these steps until all desired weights have been entered S2dV AEN SdD zn D EI Eh ia Entering Fuel Parameters SeJnpa oJd 1 Press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to place the cursor in the FUEL ON BOARD field 3 Turn the small FMS Knob to enter the desired fuel quantity 4 Press the ENT Key The cursor is now in the FUEL RESERVES field 5 Turn the small FMS Knob to enter the desi
91. ipny uddx SjueuinJjsu paezey 364 U405 AEN Wija SoJnjeoj Jeuonippy Ek aca xopu Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix MEER Index Message MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists PFD2 DB ERR PFD2 airport terrain database error exists Comments The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing PFD2 DB ERR PFD2 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists PFD2 DB ERR PFD2 Safe Taxi database error exists The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD and or PFDs detected a failure
92. ivate the WATCH feature select the WATCH Softkey This feature is only available in the Horizontal Scan Mode AFCS Weather Alert To activate or deactivate Weather Alert select the WX ALRT Softkey Activating and deactivating will also enable or inhibit the alert on the PFD GPS Nav Flight Planning Automatic Standby When the weather radar system is in the Weather or Ground Map Mode upon landing the system will automatically switch to Standby Mode Procedures TRAFFIC SYSTEMS If Traffic information Service TIS is configured a STANDBY OPERATE and TNA MUTE Softkey will be displayed Ifa Traffic Advisory System TAS is configured a STANDBY NORMAL TEST and ALT MODE Softkey will be displayed v 2 5 E a Additional Features Traffic Symbol Description Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA TAS only not available with TIS intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory TA closing rate distance and vertical separation meet TA criteria Annun Alerts Appendix QO dod Traffic Advisory Off Scale Index Traffic Symbol Description 44 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN Traffic Information Service TIS Hazard Avoidance NOTE If the G1000 is configured to use an op
93. lert Type TAWS B Page Aural Message m Pop Up Alert g Annunciation SE TAWS System Test Fail TAWS FAIL None TAWS System Failure d 3 TAWS Alerting is disabled TAWS INH None None No GPS position or TAWS N A None TAWS Not Available gt excessively degraded GPS TAWS Available E signal will be heard when sufficient GPS signalis received E System Test in progress TAWS TEST None None K System Test pass None None Chime 2 AURAL ALERTS d Aural Alert Description 3 Minimums The aircraft has descended below the preset minimum descent altitude or A decision altitude The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Vertical track aouepioay puezey Traffic Played when a Traffic Advisory TA is issued with the TIS system Traffic Not Available The aircraft is outside the Traffic Information Service TIS coverage area 2E Traffic Traffic Played when first Traffic Advisory TA is issued with an optional TAS system 2 Traffic for each subsequent TA Bs Traffic Advisory System Played when the optional KTA 870 or Skywatch HP TAS system passes a Test Passed pilot initiated self test Traffic Advisory System Played when the optional KTA 870 or Skywatch HP TAS system fails a pilot Test Failed initiated self test Skywatch System Test Played when the optional SKY497 TAS system passes a pilot
94. lerts Features Index A Additional Features GARMIN View Charts from the Active Flight Plan Page 1 2 3 4 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach Select the SHW CHRT Softkey The appropriate chart will be displayed if available for the item selected Select the GO BACK Softkey to return to the previous page Change Day Night View 1 2 3 4 5 6 7 While viewing a chart press the MENU Key to display the Page Menu OPTIONS Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options Turn the small FMS Knob to choose between the On and Off Full Screen Options Turn the small FMS Knob to choose between Day Auto and Night Options In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity Press the FMS Knob when finished to remove the Chart Setup Menu AIRPORT DIRECTORY The AOPA or AC U KWIK Airport Directory adds enhanced airport information when viewing airports on the WPT Airport Information Page The Airport Directory databases are re
95. lly displayed 5 Turn the Joystick to select the desired range 6 If desired select the VERTICAL Softkey for vertical scanning 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi AEN SdD S24V oipny uddx sjueumasuj u105 NeN 36114 Buruue d 16114 ERIT Sa1npa oJd puezey sainjea4 jeuonippy su jy unuuy x pu ddy x pul Nav Com Flight AFCS XPDR Audio Instruments GPS Nav ing Flight Plann Hazard Avoidance Procedures Additional Appendix Annun Alerts Features Index Hazard Avoidance GARMI N Adjusting Antenna Tilt Move the Joystick up or down to adjust the tilt of the antenna up or down Moni tor the displayed tilt value in the TILT field When scanning vertically a Tilt Line may be displayed to aid in positioning the tilt of the antenna If the Tilt Line is not displayed perform the following steps 1 Press the MENU Key 2 Turn the large FMS Knob to select Show Tilt Line 3 Press the ENT Key Adjusting Antenna Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left Monitor the 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 fol lowing steps 1 Press the MENU Key 2 Turn the large FMS Knob to select Show Bearing Line 3 Pr
96. ments Additional Features Appendix e Index Annunciations amp Alerts GCU 475 MESSAGE ADVISORIES A GARMIN Message GCU CNFG GCU Config error Config service req d Comments GCU 475 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GCU FAIL GCU is inoperative MANIFEST GCU software mismatch communication halted A failure has been detected in the GCU 475 The GCU 475 is unavailable The GCU 475 has incorrect software installed The G1000 system should be serviced GCU KEYSTK GCU key name Key is stuck A key is stuck on the GCU 475 bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists GMC 710 MESSAGE ADVISORIES Message Comments GMC CONFIG GMC Config error Config service req d Error in the configuration of the GMC 710 GMC FAIL GMC is inoperative A failure has been detected in the GMC 710 The GMC 710 is unavailable MANIFEST GMC software mismatch Communication halted The GMC 710 has incorrect software installed The system should be serviced GMC KEYSTK GMC key name Key is stuck 82 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi A key is stuck on the GMC 710 bezel Attempt to free the stuck key by pressing it several times The syst
97. mode selection softkeys Press the XPDR1 or XPDR2 Softkey to select the active transponder Press the CODE Softkey to display the transponder code selection softkeys for digit entry Press the digit softkeys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active ACTIVATE ADS B TRANSMIT 1 2 3 Press the XPDR Softkey to display the transponder mode selection softkeys Press the ADS B TX Softkey to enable transmission of three dimensional aircraft position and aircraft heading Press the ADS B TX Softkey again to disable transmission SELECTING A COM RADIO Transmit Receive Press the COM1 MIC COM2 MIC or COM3 MIC Key optional COM if installed on the audio panel 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 5 Sye y unuuy SoJnjee4j e uepioAy SoJnpa o0J4d Buruue d ACN Sd5 S941V oipny uadx sjueuinagsu Jeuonippy paezey fila JUI05 NEN Wila xipuaddy xopu Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index A Nav Com XPDR Audio Panel GARMIN Receive Only Press the COM1 COM2 or COM3 Key optional COM if installed on the audio panel SELECTING
98. monitor is displayed as shown in the following figure 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 99 seinpa2oJd Buruue d AEN Sd5 24V oipny uadx SjueuinJjsu fila wiop AeN fila aouepioay paezey saunyeay Jeuonippy xipuaddy su jy unuuy x pul Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index A Appendix GARMIN Uploading GRS1 Mag Var Database STARTING UPLOAD 0 07 Uploading Database to GRS1 2 When the upload is complete the prompt for the next GRS upload is displayed as seen in the following figure GRS2 MV DB Update Available Update from 2005 to 2010 DIN GRS2 Magnetic Field Variation Database Update Prompt 3 With OK highlighted press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure When the upload is complete the system is ready for use Uploading GRS2 Mag Var Database STARTING UPLOAD 6 0 Uploading Database to GRS2 100 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN A Activate a flight plan 14 Active Channel 53 Active database 97 Active Navigation Database 96 AC U KWIK Airport Directory 52 ADF 5 6 91 ADS B 93 Advisory alerts 61 AHRS 78 79 82 99 Air Data Computer 62 Airport Directory 52 Airport Signs
99. mscope lightning data from the display Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMIN Hazard Avoidance SIRIUSXM WEATHER OPTIONAL WARNING Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information contained within data link weather products may not accurately depict current weather conditions Displaying SiriusXM Weather on the Navigation Map Page 1 Select the MAP Softkey 2 Select the NEXRAD or XM LTNG Softkey to display the desired weather Select the applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 Turn the large FMS Knob to select the WPT Page Group 2 Turn the small FMS Knob to select the Airport Information Page 3 Select the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Displaying Weather on the Weather Data Link Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Data Link Page 3 Select the available softkeys to select the desired XM weather product 4 Select 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 Weathe
100. nt Pireps are displayed in yellow 68m 21000FT TURBULENCE The age of the displayed data is shown at the right The altitude selection is shown at the bottom 4m 6000FT ICING POTENTIAL The age of the displayed data is shown at the right The altitude selection is shown at the bottom 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 Ay CAUTION In Standby Mode the antenna is parked at the center line It is always a good idea to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly Displaying Weather on the Weather Radar Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turnthe small FMS Knob to select the Weather Radar Page 3 Select the MODE Softkey 4 If the aircraft is on the ground select the STANDBY Softkey to initiate the one minute warm up period After the warm up is complete the radar will enter the Standby Mode After the aircraft is airborne select the WEATHER Softkey Or If the aircraft is already airborne select the WEATHER or GROUND Softkey The one minute warm up period will be initiated after which the radar will begin transmitting The horizontal scan is initia
101. nunnunrmnunnnnun Select the BACK Softkey to return to the previous level softkeys Transponder Softkeys Level 1 Level2 Level 3 Description XPDR Displays transponder mode selection softkeys XPDRI Selects the 1 transponder as active XPDR2 Selects the 2 transponder as active STBY Selects Standby Mode transponder does not reply to any interrogations ON Selects Mode A transponder replies to inter rogations AIT Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations GND Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations VFR Automatically enters the VFR code 1200 in the U S A only CODE Displays transponder code selection softkeys 0 7 0 7 Use numbers to enter code BKSP Removes numbers entered one at a time 92 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN 11 Appendix Level 1 Level2 Level 3 Description Ha IDENT Activates the Special Position Identification s SPD pulse for 18 seconds identifying the transponder return on the ATC screen ADS B TX Activates deactivates transmission of the air crafts three dimensional position and aircraft heading for reception by ADS B systems oipny uddx U105 AEN
102. nvalid MANIFEST GRS1 software mismatch communication halted The 1 AHRS has incorrect software installed The system should be serviced MANIFEST GRS2 software mismatch communication halted The 42 AHRS has incorrect software installed The system should be serviced GMU 44 MESSAGE ADVISORIES Message Comments HDG FAULT AHRS1 magnetometer fault has occurred A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced HDG FAULT AHRS2 magnetometer fault has occurred A fault has occurred in the 2 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced MANIFEST GMU1 software mismatch communication halted MANIFEST GMU2 software mismatch communication halted The GMU 44 has incorrect software installed The system should be serviced 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 79 eouepioAy seinpa2oJd Buruue d AEN Sd5 241V oipny uddx Syueuinjjsu paezey Wij w09 eN Wija SoJnjeeoj Jeuonippy xipuaddy xopu Additional Hazard Flight Nav Com Flight Appendix Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Annunciations amp Alerts GDL 69A MESSAGE ADVISORIES A GARMIN Message GDL
103. op level softkeys aouepioay puezey Inset Map Softkeys soinjes Jeuonippy su jy unuuy D gt so o ri a E xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 87 A GARMIN Appendix z Level 1 Level 2 Description INSET Displays Inset Map in PFD lower left corner OFF Removes Inset Map 53 DCLIR 3 Selects desired amount of map detail cycles E through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data g DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan 8 WX LGND Displays icon and age on the Inset Map for the selected weather products optional TRAFFIC 2 Displays traffic information on Inset Map TRAFFIC No Traffic displayed on inset map Bf TRFC 1 Traffic displayed on inset map uu TRFC 2 Traffic Only display shown TOPO Displays topographical data e g coastlines terrain E rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map STRMSCP Press to display the Stormscope lightning data T E on the Inset Map within a 200 nm radius of the 33 aircraft NEXRAD Displays NEXRAD weather and coverage informa Eg tion on Inset Map optional feature t 8 XM LING Displays XM lightning information on Inset Map b optional feature METAR Displays METAR flags on airport symbols shown on Appendix Annun Ale
104. opu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 29 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning A GARMIN EDIT A STORED FLIGHT PLAN 1 2 3 4 5 6 1 Press the FPL Key on the Control Unit and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the EDIT Softkey Turn the large FMS Knob to place the cursor in the desired location Enter the changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or a Turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey Turn the large FMS Knob to highlight the waypoint to be deleted 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
105. or the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN 331 Appendix 14 Remove the SD card from the top card slot of the MFD 15 Turn system power ON 16 Press the ENT Key to acknowledge the startup screen 17 Turn the large FMS Knob to select the AUX Page group on the MFD 18 Turn the small FMS Knob to select the System Status Page 19 Press the Display Database Selection Softkey to show standby navigation database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct standby navigation database cycle information is shown for each display Magnetic Field Variation Database Update At startup the system compares this version of the MV DB with that presently being used by each AHRS GRS1 and GRS2 If the system determines the MV DB needs to be updated a prompt is displayed on the Navigation Map Page as shown in the following figure Note in the following example GRSI is the first AHRS to indicate an update is available In actuality this is dependent on which AHRS is the first to report status to the system GRS2 may be displayed before GRS1 The order is not important only that both AHRS be updated GRS1 MV DB Update Available Update from 2005 to 2010 OK or CANCEL GRS1 Magnetic Field Variation Database Update Prompt Loading the magnetic field variation database update 1 With OK highlighted as shown in the previous figure press the ENT Key on the MFD A progress
106. ouepioay puezey 13 soinjes Jeuonippy CREATE A USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Turn the large FMS Knob on the Control Unit to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Select the NEW Softkey A waypoint is created at the current aircraft position su jy unuuy x pu ddy 4 Enter the desired waypoint name 5 Press the ENT Key xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 21 Flight Instruments Nav Com XPDR Audio Hazard Additional AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning 6 7 8 9 A GARMIN The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select LAT LON latitude and longitude Press the ENT Key CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOIN
107. ound in preparation for takeoff GA Disengages the autopilot and commands a Switch Go Around constant pitch attitude and wings level in GA the air Level Commands 0 pitch attitude SERA WL ALTS armed automatically when PIT VS FLC TO or GA active and under VPTH when Selected Altitude is to be captured instead of VNAV Target Altitude ATTV armed automa ically ui Go Around mode disengages the autopilot unless a compatible lift computer is installed 22 T evel mode can only become activated as a function of Electronic Stability and Protection ESP 10 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi ider VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude 190 00664 02 Rev B A GARMIN 1 AK LATERAL MODES sjueuinijsu ufi Lateral Mode Description Control Annunciation Holds current aircraft roll attitude Roll Hold or rolls wings level depending on default ROL commanded bank angle SE Ja E DO eg Sel o Limits maximum commanded roll BANK Low Bank angle Key Captures and tracks Selected Heading Select Heading HDG Key HDG avigation GPS Arm GPS Capture Track D avigation VOR Enroute AmyCapture Tiadk Captures and tracks selected NAV Key VOR navigation source GPS VOR LOC avigation LOC Arm Capture Track LOC No Glideslope Buruue d 164 Backcourse Arm Capture Cap
108. played in the GAIN field Ground Mapping 1 Select th 2 Select the GROUND Softkey to place the radar in Ground Map Mode 3 Selectth Sector Scan e MODE Softkey e BACK Softkey 1 While in the Horizontal Scan Mode move the Joystick right or left to place the Bearing Line in the desired position The location of the Bearing Line will become the center point of the Sector Scan 2 Press the FMS Knob to display the cursor 3 Turn the large FMS Knob to place the cursor in the SECTOR SCAN field 4 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 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 43 AEN SdD S24V oipny uadx sjueumasuj u105 AeN fila Buruuejd 1ufil4 ERIT SaJnpa oJd puezey sainjea4 jeuonippy su jy unuuy xipuaddy xopu Hazard Avoidance GARMI N Antenna Stabilization 1 To activate or deactivate the antenna stabilization select the MODE Softkey 2 Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softkey to deactivate The current stabilization condition is shown in the upper right of the weather radar display Flight Instruments Nav Com XPDR Audio Weather Attenuated Color Highlight WATCH To activate or deact
109. pplied between 30 and 75 The force increases as roll attitude increases and decreases as roll attitude decreases The applied force is intended to encourage pilot input that returns the airplane to a more normal roll attitude As roll attitude decreases ESP will disengage at 30 ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement attitude limit of 75 GPS Nav AFCS Flight Planning Pitch Engagement ESP engages at 17 nose up and 15 nose down Once ESP is engaged it will apply increasing opposing force between 17 and 20 nose up and between 15 and 18 nose down Maximum opposing force is applied between 20 and 50 nose up and between 18 and 50 nose down ESP disengages when 50 is exceeded in a nose up or nose down attitude With ESP engaged and the aircraft in a nose up condition opposing force steadily decreases from 20 nose up to 15 nose up as aircraft pitch moves toward zero degrees ESP disengages at 15 nose up With ESP engaged and the aircraft in a nose down condition opposing force steadily decreases from 18 nose down to 13 nose down as aircraft pitch moves toward zero degrees ESP disengages at 13 nose down The opposing force increases or decreases depending on the pitch angle and the direction of pitch travel This force is intended to encourage movement in the pitch axis in the direction of the normal pitch attitude range for the aircraft
110. r Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to place the panning arrow on AIRMETs TFRs METARS or SIGMETs 3 Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 39 AEN SdD S24V oipny uadx sjueumasuj u105 NeN fila Buruuejd 16114 ERIT SaInpa oJd puezey sainjea4 jeuonippy su jy unuuy x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Additional Appendix Annun Alerts Features Avoidance Procedures GPS Nav AFCS Index Hazard Avoidance A GARMIN Weather Products and Symbols Wx Product Status Icons Description US 3m CN Bm NEXRAD Available for the US and Canada The age of the displayed data for each is shown at the right b 5m ECHO TOP The age of the displayed data is shown at the right Not displayed when CLOUD TOP is displayed p 12m CLOUD TOP The age o
111. red reserve fuel quantity 6 Press the FMS Knob to remove the cursor 7 Press the ENT Key TRIP PLANNING SoJnjeeo4 e uepioAy paezey Jeuonippy su jy unuuy 1 Turn the large FMS Knob on the Control Unit to select the AUX page group 2 Turn the small FMS Knob to select the Trip Planning Page 3 The current PAGE MODE is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode select the AUTO or MANUAL Softkey xipuaddy xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 19 Flight Instruments Nav Com XPDR Audio Hazard Additional AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning 4 For a b c d Or For a b c d Or A GARMIN Direct to planning Select the WPTS Softkey and verify that the starting waypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint point to point planning Enter the identifier of the starting waypoint Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending wa
112. rom published localizer course by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS Selected course for LOC2 differs from published localizer course by more than 10 degrees PFD1 PFD2 or MFD1 CARD 1 REM Card 1 was removed Reinsert card The SD card was removed from the top card slot of the specified PFD or MFD The SD card needs to be reinserted PFD1 PFD2 or MFD1 CARD 2 REM Card 2 was removed Reinsert card The SD card was removed from the bottom card slot of the specified PFD or MFD The SD card needs to be reinserted PFD1 PFD2 or MFD1 CARD 1 ERR Card 1 is invalid The SD card in the top card slot of the specified PFD or MFD contains invalid data PFD1 PFD2 or MFD1 CARD 2 ERR Card 2 is invalid The SD card in the bottom card slot of the specified PFD or MFD contains invalid data 86 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 190 00664 02 Rev B GARMIN Appendix APPENDIX Ssjueuinisu iui PFD SOFTKEY MAP optional nanos DD nononos an oipny uddx U105 AEN CDI NAV1 Top Level PFD Softkeys 3 optional L psnumuannnntunnon Buruue d 1614 optional optional optional TERRAIN STRMSCA NEXRAD xv LING ALERTS F F3 rr nnn i 9 3 s e E D E J gt zu a E Gis UU fe SeJnpa oJ4d Select the BACK Softkey to return to the t
113. ror exists Comments The MFD and or PFD detected a failure in the basemap database MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists PFD2 DB ERR PFD2 terrain database error exists The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists the system should be serviced MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing PFD2 DB ERR PFD2 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists PFD2 DB ERR PFD2 obstacle database error exists The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 obstacle database missing database missing PFD1 DB ERR PFD1 obstacle PFD2 DB ERR PFD2 obstacle database missing The obstacle database is present on another LRU but is missing on the specified LRU 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 69 eouepioAy seinpa2oJd Buruue d AEN Sd5 241V o
114. rts Index the Inset Map optional 88 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN 11 Appendix optional INSET SENSOR XPDR IDENT MR REF NRST ALERTS 2 am LA T S D n OD 3 S D nn 23 a a Apc1 bc2 amp Rs1 AHRS2 fl lI Back _ aLeRTs FX V3 V3 V3 V3 V3 V3 P3 P3 w Select the BACK Softkey to return to the top level softkeys oipny uddx U105 AEN Sensor Softkeys E Level 1 Level2 Description SENSOR Displays softkeys for selecting the 1 and 2 AHRS 2 and Air Data Computers g ADCI Selects the 41 Air Data Computer ADC2 Selects the 2 Air Data Computer Buruue d 164 AHRSI Selects the 1 AHRS AHRS2 Selects the 2 AHRS s n e 4 aouepioay saunpar0ld puezey Jeuonippy su jy unuuy D gt so 3 a E xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 89 Additional Hazard Flight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index A Appendix COG ARMIN mn npnununanunnniuon cU swws orus wo owe erat Hsrewr ence aAcruwr sro Bano Back ALeRTS P FK P Nn E amp v1 m t BRGANWI Select the BACK Softkey to return to the top level softkeys BRG2 GPS BRG2 ADP J OOO os peces 1
115. s now displayed only as a reference It will not be used to give flight path vertical guidance Other displayed altitudes may change due to re calculations or rendered invalid as a result of manually changing an altitude to a non designated altitude White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by Altitude has been The system cannot the system estimating entered by the pilot use this altitude in the altitude of the Altitude is designated determining vertical Small Text aircraft as it passes over the navigation point This altitude is provided as a reference and is not designated to be used in determining vertical flight path guidance Altitude is not designated to be used in determining vertical light path guidance Altitude has been retrieved from the navigation database and is provided as a eference n for use in giving vertical flight path guidance Altitude does not match the published altitude in navigation database or no published altitude exists Altitude is designated for use in giving vertical flight path guidance Altitude has been etrieved from the navigation database or has been entered by the pilot and matches a published altitude in the navigation database flight path guidance The system cannot use this altitude in determining vertical flight path guidance 16 Garmin G1000 Cockpit Reference Guide for the
116. sed UNABLE V WPT Can t reach current vertical waypoint The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints The system automatically transitions to the next vertical waypoint VNV Unavailable Unsupported leg type in flight plan The lateral flight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Excessive crosstrack error The current crosstrack exceeds the limit causing 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 Doox The position of the selected waypoint xxxx is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed Do not use GPS to navigate to the selected non WGS84 waypoint TRAFFIC FAIL Traffic device has failed The system is no longer receiving data from the traffic system The traffic device should be serviced STRMSCP FAIL Stormscope has failed Stormscope has failed The system should be
117. struments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional AFCS GPS Nav Procedures Appendix Annun Alerts Features Index A GARMIN AFCS VERTICAL MODES Vertical Mode Description Control Annunciation Holds the current aircraft pitch attitude may Pitch Hold be used to climb descend to the Selected default PIT Altitude Selected Altitude AFCS armed to capture the altitude displayed in x ALTS Armed the Selected Altitude window Altitude Hold Holds the current Altitude Reference ALT Key AIT nnnnnrr Maintains the current aircraft vertical Vertical Speed speed may be used to climb descend to the VS Key VS nnnn rem Selected Altitude Flight Level Change Maintains the current aircraft airspeed in IAS Hold IAS or Mach while the aircraft is dimbing FLC LUE descending to the Selected Altitude Press FLC Key Flight Level Change the SPD Key to switch between IAS and FIC M nnn ach Hold MACH VNAV Captures and tracks the VNAV flight path VNV Key VPTH AFCS armed to capture the altitude VNAV Target j Alsitide Armed displayed in the VNAV Target Altitude ALTV window Glidepath Captures and tracks the SBAS glidepath on GP approach C d tracks the ILS glides ea Glideslope aptures and tracks the ILS glideslope on GS approach Disengages the autopilot and commands a Takeoff constant pitch angle and wings level in the TO air on the gr
118. t Press the ENT Key to advance to the next checklist Select the RETURN Softkey to return to the previous checklist Select the EXIT Softkey to exit the Checklist Page and return to the page last viewed Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS G1000 SYSTEM ANNUNCIATIONS When an LRU or an LRU function fails a large red X is typically displayed on windows associated with the failed data Refer to the AFM for additional information regarding pilot responses to these annunciations System Annunciation Comment Attitude and Heading Reference System is aligning Display system is not receiving attitude information from the AHRS GPS information is either not present or is invalid for navigation use Note that AHRS utilizes GPS inputs during normal operation AHRS operation may be degraded if GPS signals are not present see AFM Display system is not receiving valid heading input from AHRS Display system is not receiving valid transponder information 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi Sa1npa2old Buruue d AEN Sd5 S 041V oipny uddx sjueumnasu fila wiop AeN fil aouepioay paezey soinjes4 Jeuonippy T acu xopu A Annunciations amp Alerts GARMIN G1000 SYSTEM ANNUNCIATIONS CON
119. t C90A GT GTi 190 00664 02 Rev B A GARMIN GTX 33 MESSAGE ADVISORIES Annunciations amp Alerts Message XPDR1 CONFIG XPDR1 config error Config service req d Comments The transponder configuration settings do not match those of backup configuration memory The system should be serviced XPDR2 CONFIG XPDR2 config error Config service req d The transponder configuration settings do not match those of backup configuration memory The system should be serviced MANIFEST GTX1 software mismatch communication halted The transponder has incorrect software installed The system should be serviced MANIFEST GTX2 software mismatch communication halted The transponder has incorrect software installed The system should be serviced XPDR1 SRVC XPDR1 needs service Return unit for repair The 1 transponder should be serviced when possible XPDR2 SRVC XPDR2 needs service Return unit for repair The 2 transponder should be serviced when possible XPDR1 FAIL XPDR1 is There is no communication with the 1 inoperative transponder XPDR2 FAIL XPDR2 is There is no communication with the 2 inoperative transponder 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 71 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx SyueuinJjsu paezey Wij w09 eN 1014 SoJnjeo4j Jeuonippy
120. t Type TAWS B Page Aural Message Ma Pop Up Alert Annunciation Imminent Obstade PULL UP Obstacle Ahead Pull Up Impact Warning or Obstacle Ahead Pull Up 0 Obstacle Obstacle Pull Up Pull Up Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Clearance or Terrain CART TERRA EAD T Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN TERRAIN AHEAD Terrain Ahead Terrain Impact Caution ITI or Ahead CAUTION TERN I Caution Terrain Caution Terrain Reduced Required TERRAIN cauow oBsrAcLE Caution Obstacle Cau Obstacle Clearance or tion Obstacle Caution ROC STALE AHEAD o Obstacle Ahead Obstacle Ahead Imminent Obstacle TERRAIN OBSTACLE AHEAD Obstacle Ahead Obstacle Impact Caution IO or Ahead CAUTION OBSTACLE i Caution Obstacle Caution Obstacle Premature Descent TERRAIN TOO LOW TERRAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Five Hundred 500 Excessive Descent TERRAIN SIKRE Sink Rate Rate Caution EDR Negative Cimb TERRAIN m Don t sink Rate Caution NCR or or aeee Teolow Tern 64 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 190 00664 02 Rev B A GARMIN Annunciations amp Alerts TAWS System Status Annunciations Ssjueuinijsu ufi PFD MFD MFD A
121. t to Navigation from the MFD 1 Press the Direct to IJ Key on the Control Unit 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 5 Turn the large FMS Knob to place the cursor over the VNV altitude field 6 Enter the desired altitude 7 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 9 8 Turn the small FMS Knob to select MSL or AGL 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field 10 Enter the desired offset distance before or after the waypoint 11 Press the ENT Key The Activate field is highlighted 12 Press the ENT Key to activate Direct to Navigation from the PFD 1 Press the Direct to Key J on the PFD 2 Turn the large FMS Knob to place the cursor in the desired selection field GPS Navigation 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob to place the
122. ted in the following table when the flight director is not active activates the pilot side flight director in the listed modes ACN Sd5 Modes Selected Control Pressed Lateral Vertical E FD Key Roll Hold default ROL Pitch Hold default Pr ES AP Key Roll Hold default ROL Pitch Hold default PIT CWS Button Roll Hold default ROL Pitch Hold default PIT i Takeoff on ground TO Takeoff on ground TO 8 SSMUS Go Around in air GA Go Around in air GA ALT Key Roll Hold default ROL Altitude Hold ALT H F VS Key Roll Hold default ROL Vertical Speed VS 8 VNV Key Roll Hold default ROL Vertical Path Tracking VPTH GPS ze NAV Key Navigation VOR Pitch Hold default PIT 3 amp 8 LOC BC Key Backcourse BC Pitch Hold default PIT i GPS Pitch Hold default PIT d APR Key Approach VAPP Glidepath GP LOC Glideslope GS HDG Key Heading Select HDG Pitch Hold default PIT a Valid VNV flight plan must be entered before VNV Key press activates flight director The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAV or APR Key press activates flight director ys selected navigation receiver must have a valid LOC signal before BC Key press activates flight irector xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 9 Flight In
123. thin their respective engagement limits ESP can also be overridden by overpowering the servos mechanical torque limit ESP can be enabled or disabled on the AUX SYSTEM SETUP 2 Page on the MFD To enable or disable ESP 1 Turn the large FMS Knob to select the AUX Page Group 2 Turn the small FMS Knob to select the System Setup Page 3 f necessary select the SETUP 2 Softkey to display the AUX SYSTEM SETUP 2 Page If the AUX SYSTEM SETUP 2 is already displayed proceed to step 4 4 Press the FMS Knob to activate the cursor 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 55 sainpa0ld Buruue d AEN Sd5 S 041V oipny uddx sjueuimasu fila u105 NeN fila aouepioay puezey xipuaddy su jy unuuy s N e 4 Jeuonippy xepu Additional Features GARMI N 5 Turn the large FMS Knob to place the cursor in the STABILITY amp PROTECTION field 6 Turn the small FMS Knob to select ENABLE or DISABLE 7 Press the FMS Knob to remove the cursor Flight Instruments Nav Com XPDR Audio Roll Engagement Roll Limit Indicators are displayed on the roll scale at 45 right and left indicating where ESP will engage As roll attitude exceeds 45 ESP will engage and the on side Roll Limit Indicator will move to 30 The Roll Limit Indicator is now showing where ESP will disengage as roll attitude decreases to within the desirable roll attitude range Once engaged ESP force will be a
124. tion database as the active database prior to its effective date will result in the expiration date on the power up screen and the effective date on the AUX System Status Page being displayed in yellow NOTE After the navigation database is loaded or copied the top SD card may be removed With the system OFF insert the SD card containing the new navigation database version into the top card slot of the display PFD1 PFD2 or MFD to be updated label of SD card facing left Turn the system ON A prompt is displayed in the upper left corner of the display Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN 1 33 Appendix DO YOU WANT TO UPDATE THE STANDBY NAVIGATION DATABASE ON THE BOTTOM CARD THE STANDBY DATABASE WILL BE ACTIVATED UPON THE FIRST ON GROUND POWER CYCLE ON OR AFTER 80 00 SYSTEM TIME ON THE EFFECTIVE DATE FROM REGION WORLDWIDE WORLDWIDE sjueuinisu fid CYCLE 1284 1285 EFFECTIVE 9 APR 2012 7 MAY 2612 EXPIRES 7 MAY 2812 84 JUN 2812 NO WILL BE ASSUMED IN 21 SECONDS oipny uddx U105 AEN 3 Pressthe NO Softkey to proceed to loading the active database 4 Aprompt similar to the following is displayed Press the YES Softkey to update the active navigation database S2dV DO YOU WANT TO UPDATE THE ACTIVE NAVIGATION DATABASE SELECTING YES WILL OUERHRITE THE ACTIVE NAVIGATION DATABASE FROM TO WORLDWIDE WORLDWIDE 12804 12805 A
125. tional Traffic Advisory System TAS TIS is not available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page 1 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page Select the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select the STANDBY Softkey to place the system in the Standby Mode STANDBY will be displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Select the TNA MUTE Softkey to mute the Traffic Not Available aural alert Displaying Traffic on the Navigation Map 1 2 Ensure TIS is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic will now be displayed on the map Traffic Advisory System TAS Optional System Self Test 1 2 3 4 Set the range to 2 6 nm Select the STANDBY Softkey Select the TEST Softkey Self test will take approximately eight seconds to complete When completed successfully traffic symbols will be displayed and a voice alert appropriate for the installed system will be heard indicating the test passed see Annuciations amp Alerts
126. tions amp Alerts Message ADC1 ALT EC ADCI altitude error correction is unavailable ADC2 ALT EC ADC altitude error correction is unavailable Comments GDC1 or GDC2 is reporting that the altitude error correction is unavailable ADC1 AS EC ADC1 airspeed error correction is unavailable ADC2 AS EC ADC airspeed error correction is unavailable GDC1 or GDC2 is reporting that the airspeed error correction is unavailable ADC1 Service ADC1 needs service Return unit for repair ADC2 Service ADC2 needs service Return unit for repair A failure has been detected in the GDC1 or GDC2 The system should be serviced MANIFEST GDC1 software mismatch communication halted MANIFEST GDC2 software mismatch communication halted The GDC 74B has incorrect software installed The system should be serviced MANIFEST ADC1 software mismatch communication halted MANIFEST ADC software mismatch communication halted The GDC1 and or GDC2 self test has detected a problem in the unit The system should be serviced 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 81 eouepioAy senpa2o0Jd Buruue d AEN Sd5 241V oipny uddx SjueuinJjsu paezey Wija w09 eN Wija SoJnjeo4j Jeuonippy Dun asdf xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instru
127. tivate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 1 N 3 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint Select the ACT LEG Softkey OR Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMIN Navigation STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL Key on the Control Unit to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to delete the flight plan This will not delete the stored flight plan only the active flight plan sjueuinisu fi oipny uddx U105 AEN VERTICAL NAVIGATION VNAV S2dV The navigation database only contains altitudes for procedures that call for Cross at altit
128. to select the desired waypoint Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position oipny uddx U105 AEN S2dV Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints AEN Sd5 zn gt EI Eh ia Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Press the ENT Key Repeat step 10 to enter the next waypoint name Press the ENT Key The cursor is displayed in the RAD radial field for the second waypoint Enter the desired radial from the reference waypoint 15 Press the ENT Key 16 Press the FMS Knob to remove the flashing cursor aouepioay saunpar0ld puezey soinjes Jeuonippy 11 su jy unuuy 1
129. tures and tracks a localizer Trac signal for backcourse approaches BER a 3 Approach GPS Arm Capture GPs 8 rac Approach VOR Arm Capture gt a VAPP Si rac Captures and tracks selected EE a APR Key 3d Approach ILS Arm Capture navigation source GPS VOR LOC s rac LOC Glideslope Mode ge automatically armed d Commands a constant pitch angle Takeoff and wings level in preparation for TO gt takeoff GA 5 Commands a constant pitch ange a 2 Go Around ommands a constant pitch angle GA E and wings level in the air Level Commands wings level attitude didi LVL E No annunciation as in the AFCS Status Box The acceptable bank angle range is indicated in green along the Roll Scale of the Attitude Indicator Go Around mode disengages the autopilot unless a compatible lift computer is installed x pul Level mode can only become activated as a function of Electronic Stability and Protection ESP 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 11 GARMIN AFCS Sjueuinijsu iui oipny uddx wo gt AeN S24V ACN Sd5 buruue d Wila Blank Page s np Old e uepioAy piezed so1njea4 Jeuonippy Syo v unuuy xipuaddy xopu Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft COOA GT GTi 190 00664 02 Rev B 12 A GARMIN GPS NAVIGATION DIRECT TO NAVIGATION Direc
130. udes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually KI DFW z oz E 5 gt e Mag ST arcc Whi COVIE 221 9 0NM 12400FT ai 3 LEMYN 220 80w MCS ae Large Light 2 Li Blue Text 8 Approach KDFW RNAV 17LePs LPV RIVET iaf EN NE Small Light DRAAK BEEN 66 EE INWOD 3 2NM Sma Lg t 8 MENOL fof 39MM Zammer le Subdued RW17L KIT ge i d Small White Text SE 99 FT 8NM with Altitude amp si POLKE Restriction Bar gt a RISE Cross AT or ABOVE 5 000 fi z Fac Cross AT 2 300 fi ICE M Cross AT or BELOW 3 000 ft xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 15 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional AFCS Appendix Annun Alerts Features Avoidance Procedures Index GPS Navigation A GARMIN Altitudes associated with arrival and approach procedures are auto designated This means the system will automatically use the altitudes loaded with the arrival or approach for giving vertical flight path guidance outside the FAF Note that these alti tudes will be displayed as small light blue text Altitudes that have been designated for use in vertical navigation may also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key The altitude i
131. unctional It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features If an error occurs during synchronization an error message will be displayed followed by the affected display in the Sync Status section of the Database Window If synchronization completes on one display but an error occurs on another the error message will be displayed with the affected displays listed after it When an error message is displayed the problem must be corrected before synchronization can be completed A power cycle is required to restart synchronization when Card Full or Err is shown Error Message Description Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted Timeout System timed out prior to the database transfer completing 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 95 sainjea4 aouepioay saunpa20ld Buruue d AEN Sd5 24V oipny uddx sjueumnansu puezey wo gt AeN Jeuonippy su jy unuuy gt so F a E xopu fila 1614 Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Annun Alerts
132. vised every 56 days Check fly garmin com for the current database View Airport Directory Information 52 While viewing the WPT Airport Information Page if necessary select the INFO 1 Softkey to change the softkey label to display INFO 2 Airport Directory information is displayed on the right half of the display Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B A GARMIN ____ Adiitional Features SIRIUSXM SATELLITE RADIO The XM Radio Page provides information and control of the audio entertainment features of the SiriusXM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select the displayed AUX XM Information Page 3 Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio 1 Select the CATGRY Softkey on the XM Radio Page 2 Select the CAT and CAT softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with th
133. window will be displayed With ACTIVATE highlighted press the ENT Key Or Press the go around button 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi Procedures 35 AEN SdD S24V oipny uadx sjueumasuj u105 NeN fila Buruuejd 16114 SoJnpa oJd su jy unuuy sainjea4 aouepioay jeuonippy paezey xipuaddy xopu Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Procedures 36 Blank Page Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi A GARMIN 190 00664 02 Rev B GARMIN Hazard avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page STORMSCOPE OPTIONAL WARNING The Stormscope system is not intended 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 deta
134. y to use the software or re esentative has been advised o ter collectively included in this bility erwise Under idental special or ated f the extent allowed ated ages vely AC U KWIK Organization to the AC U KWIK information included imited to the implied warranties of f ormation is provided as is a WIK Organizations and to the ess AC U KWIK Organizations tual or alleged inaccurac in the datasets Some ju es or liability for incident isdicti al or nsee S nd esentations regarding its accuracy ies in the ons Printed in the U S A A GARMIN Waminps Cautions amp Notes WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The terrain avoidance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes
135. y uddx U105 AEN SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG Push the BARO Knob to select standard pressure S2dV CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Press the PFD Softkey to display the second level softkeys 2 Press the ALT UNIT Softkey 3 Press the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Press the HPA Softkey to display the barometric pressure setting in hectopascals 4 Press the BACK Softkey to return to the top level softkeys Bujuueld AEN Sd5 164 SeJnpa oJd SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS aouepioay puezey 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight BARO in SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF sainjes Jeuonippy su jy unuuy SYNCHRONIZE CDI 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF xipuaddy xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 1 Nav Com XPDR Audio Flight Planning Hazard Additional AFCS GPS Nav Appendix Annun Alerts Features Avoidance Procedures Index A Flight
136. yed 3 DME Displays the DME Information Window BRGI Cycles the Bearing 1 Information Window through NAVI or GPS waypoint identifier and GPS derived distance information and ADF frequency HSI FRMT Displays the HSI formatting softkeys 360 HSI Displays the HSI in a 360 degree format ARC HSI Displays the HSI in an arc format BRG2 Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information and ADF frequency seinpa2o0Jd Buruue d 16114 aouepioay puezey ALT UNIT Displays softkeys for setting the altimeter and BARO settings to metric units METERS When enabled displays altimeter in meters saunyeay Jeuonippy su jy unuuy IN Press to display the BARO setting as inches of mercury HPA Press to display the BARO setting as hectopacals gt kej a Ej STD BARO Sets barometric pressure to 29 92 in Hg 1013 hPa xopu 190 00664 02 Rev B Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT GTi 91 Additional Hazard Flight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index A Appendix 5 GARMIN optional nmpmnsnnn 9n npsmsnun XPDR1 XPDR2 STBY ON ALT GND VFR CODE IDENT ADS BTX BACK ALERTS F3 F3 Fr n n F3 V3 rn Select the BACK Softkey to return to the top level softkeys IEEE IE IE HE EA Tes E88 TIERS pnnmumnu
137. ypoint Again enter the identifier of the ending waypoint Press the ENT Key to accept the waypoint For flight plan leg planning a b c d Select the FPL Softkey at the bottom of the display Turn the small FMS Knob to select the desired flight plan already stored in memory by number Turn the large FMS Knob to highlight the LEG field Turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan Selecting FPL 00 will display the active flight plan If an active flight plan is selected REM will be an available option to display planning data for the remainder of the flight plan NOTE The page mode must be set to MANUAL to perform the following steps Turn the large FMS Knob to highlight the departure time DEP TIME field NOTE The departure time on the Trip Planning Page is used for preflight planning Refer to the Utility Page for the actual flight departure time Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft CO0A GT GTi 190 00664 02 Rev B GARMIN Flight Planning 6 Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings sjueuinisu fid 7 The flashing cursor moves to the ground speed GS field Enter the ground speed Press the ENT Key when finished Note that in automatic

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