Home

Garmin Software Version 0636.02 Cockpit Reference Guide

1. sssssssseeeee nnn Reversionary Sensor Annunciations ARCS Aleris r n s ERU TAWS Alerts Lee de odio bereiten a d d Aural Alerts sss Flight Plan Import Export Messages MFD amp PFD Message Advisories Database Message Advisories GMA 1347D Message Advisories GIA 63W Message 50 1165 GEA 71 Message Advisories ssssssssseeee nne GTX 33 Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories GDL 69A Message Advisories sss GWX 68 Alert Messages GDC 74B Message Advisories GCU 475 Message Advisories GMC 710 Message Advisories Miscellaneous Message Advisories sssssse APPENDIX a e Pe it PFD Softkey Map MFD Softkey 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT l Table of Contents GARMI N Blank Page iv Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A GARMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING a 8 g x 3 o FA i Turn the BARO Knob to select the desired setting oipny uddx u102 AEN SELECTING STANDARD BAROMETRIC PRESSURE 29
2. 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 DOVVN 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 INDIVIDUALLY 1 2 3 4 Press the TMR REF Softke
3. 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 XM RADIO ENTERTAINMENT 50 The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Page 1 2 3 Turn the large FMS Knob to select the Auxiliary Page Group Turn the small FMS Knob to select the displayed AUX XM Information Page Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN S l bnsl Features 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 K
4. Pight Planning IMPORT A FLIGHT PLAN FROM AN SD CARD sjueuinisu fid 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 5 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 the ENT Key 52 AEN 540 EU e a o Qa 2 E o aouepioay puezey INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN SoJnjeej 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 wayp
5. 190 00664 01 Rev A A GARMIN Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES Message DATA LOST Pilot stored data was lost Recheck settings Comments The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings if 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 PFD2 config error Config service req d The PFD configuration settings do not match backup configuration memory The system should be serviced MFD1 CONFIG MFD1 config error Config service req d SW MISMATCH GDU software version mismatch Xtalk is off The MFD configuration set
6. 4 Activate a Flight Plan Leg 4 Stop Navigating a Flight Plan 5 Vertical Navigation 5 5 FLIGHT PLANNING LA b daz 7 Weight Planning tnter nce tn ttt ntn m Ahu d 7 Trip Planning nennen 7 Create a New User Waypoint Defined by Latitude amp Longitude 9 Create a New User Waypoint Defined by Radials from Other Waypoints 20 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT Table of Contents GARMI N Create a New User Waypoint Defined by a Radial amp Distance from Another 6665622000 00000 000 Delete a User Waypoint Create a New 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 2 Store a Flight Plan roter teta een Edit a Stored Flight Plan Delete a Waypoint from the Flight Plan sss Invert and Activate a Stored Flight Plan Copy a Flight Plan eret eret ende Delete a Flight Plan ttt rd Graphical Flight Plan Creation sse Export a Flight Plan to an SD PROCEDURES a aaa
7. 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 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 67 eouepioAy seinpa2oJd Buruue d AEN Sd5 241V oipny uddx SjueuinJjsu paezey Wija U405 AEN UTE SoJnjeej Jeuonippy 5 x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts A GARMIN GTX 33 MESSAGE ADVISORIES CONT Message XPDR1 SRVC XPDR1 needs service Return unit for repair Comments 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 is There is no communication with the 1 inoperative transponder XPDR2 FAIL XPDR2 is There is no communication with the 2 inoperative transponder GRS 77 MESSAGE ADVISORIES Messag
8. 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 Tum 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 window will be displayed With ACTIVATE highlighted press the ENT Key Or Press the go around button 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT Procedures 33 AEN 540 S24V oipny uadx sjuoumnasuj u105 NeN fila SoJnpa oJd su jy unuuy sainjea4 aouepioay jeuonippy paezey xipuaddy x
9. Terrain Clearance or Terrain Camon g 5 T Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN TERRAIN AFAD Terrain Ahead Terrain Impact Caution ITI or Ahead CATION 9 i Caution Terrain Caution Terrain Reduced Required TERRAIN CAUTION OoBsTACLE Caution Obstacle Cau Obstade Clearance or tion Obstade Caution ROC BHB o Obstacle Ahead Obstacle Ahead Imminent Obstacle TERRAIN OBSTACLE AHEAD Obstacle Ahead Obstacle Impact Caution 101 or Ahead CATION OBSTACLE i Caution Obstacle Caution Obstacle Premature Descent TERRAIN TOO 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 Too Low Tern 56 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN Annunciations amp Alerts TAWS System Status Annunciations sjueuinijsu ufi PFD MFD MFD Alert Type TAWS B Page Aural Message 5 Pop Up Alert S Annunciation SE TAWS System Test Fail 5 FAIL None TAWS System Failure 2 3 TAWS Alerting is disabled TAWS INH None None No GPS position or TAWS N A None TAWS Not Avai
10. mismatch communication halted A failure has been detected in the GDL 69 The receiver is unavailable The system should be serviced The GDL 69 has incorrect software installed The system should be serviced 70 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN GWX 68 ALERT MESSAGES Annunciations amp Alerts Message GWX CONFIG GWX config error Config service req d Comments 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 Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm GDC 74B MESSAGE ADVISORIES Message Comments ADC1 ALT EC ADCI altitude error correction is unavailable ADC2 ALT EC ADC altitude error correction is unavailable GDC1 or GDC2 is reporting that the altitude error correction is
11. pul Additional Hazard Fight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Procedures 34 Blank Page Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT A GARMIN 190 00664 01 Rev A GARMIN Hazard avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 2 3 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 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 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 detailed operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 2 Press the MAP Softkey 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 Strike is between 6 and 60 seconds old EH Strike is between 1 and 2 minutes
12. 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 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 5 SH ly unuuy sainjea4 aouepioay saunpa20ld Buruue d AEN Sd5 2 4 s u uinnsu jeuonippy p ezeH ifi U05 AEN Wija x pu ddy x pul Additional Hazard Flight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index A Nav Com XPDR Audio Panel GARMIN Receive Only Press the COM1 COM2 or COM3 Key optional COM if installed on the audio panel SELECTING A NAV RADIO 1 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VOR1 LOC1 NAV1 or VOR2 LOC2 NAV2 2 Press the NAV1 NAV2 DME or ADF Key on the audio panel to select or deselect 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 ra
13. xxxx The selected waypoint box does not use the WGS 84 datum Cross check position with alternate navigation sources 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 61000 system should be serviced FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63 W has failed 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 75 seinpa2oJd Buruue d AEN Sd5 24V oipny uddx SjueuinJjsu paezey Wij w09 eN Wij SoJnjeeoj Jeuonippy i EA x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix eee Index Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message MAG VAR WARN Large magnetic variance Verify all course angles Comments 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
14. 2 Air Data Computer HRS 2 AHRS 1 GPS 2 GPS AFCS ALERTS Condition Annunciation Description Pitch Failure PTCH Pitch axis control failure Roll Failure ROLL Roll axis control failure Pitch Trim Axis If annunciated when AP is engaged a failure has occurred in Control Failure the pitch trim system 77 YD control failure System Failure AFCS 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 Down A condition has developed causing the pitch servo to provide a sustained force in the nose down direction 54 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A GARMIN Amunciations amp Alerts Condition Annunciation Description 2 Aileron Mistrim A condition has developed causing the roll servo to provide a Left a sustained left force Aileron Mistrim A condition has developed causing the roll servo to provide Sz Right a sustained right force 5 Left provide a sustained force Rudder Mistrim Right Preflight Test A condition has developed causing the yaw servo to provide a sustained force 52 Rudder Mistrim E RUD A condition has developed causing the yaw servo to PFT Performing preflight system test Upon completion of the test the aural alert will b
15. 3 Select the BACK Softkey 8 Sector Scan 1 While in the Horizontal Scan Mode move the Joystick right or left to place z the Bearing Line in the desired position The location of the Bearing Line i will become the center point of the Sector Scan 5 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 Tum the small FMS Knob to select FULL 60 40 or 20 scan M 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 Additional Features Antenna Stabilization 1 Annun Alerts 2 Appendix To activate or deactivate the antenna stabilization select the MODE Softkey 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 Weather Attenuated Color Highlight WATCH Index 44 To activate or deactivate the WATCH feature select the WATCH Softkey This feature is only available in the Horizontal Scan Mode Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A GARMIN 3 Hazard avoidance VVeather Alert To activate or deactivate VVeather Alert select the VVX ALRT Soltkey Activating and deactivating will also enable or inhibit the alert on the PFD sjueuinisu iui Automati
16. 92 IN HG Push the BARO Knob to select standard pressure 52 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 1614 s inp old SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS 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 soinjeo Jeuonippy SH ly 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 x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 1 Nav Com XPDR Audio Flight Planning Hazard Additional AFCS GPS Nav Appendix Annun Alerts Features Avoidance Procedures Index A Flight Instruments GARMIN CHANGE NAVIGATION SOURCES 1
17. A FLIGHT PLAN oipny uddx J05 AEN 52 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 Get e a o a 2 E o 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 SoJnjeoj 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 pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 2 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning A GARMIN EDIT A STORED FLIGHT PLAN
18. Load and Activate a Departure Procedure Activate A Departure Leg Load An Arrival Procedure Activate An Arrival Leg Load and or Activate an Approach Procedure Activate An Approach in the Active Flight Plan Activate a Vector to Final Approach Fix sss Activate A Missed Approach in the Active Flight 77 6 5 HAZARD AVOIDANCE nn 35 Customizing the Hazard Displays on the Navigation 35 STORMSCOPE Optional v 35 XM Weather Optional Traffic Systems SAR lila uo Pam HE ien d edil Terrain Awareness amp Warning System TAWS 1 40 Airborne Color Weather Radar 42 ADDITIONAL FEATURES Synthetic Vision Terminal Procedure Charts XM Radio Entertainment ssssseeeeennnene Garmin 61000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN Contents ANNUNCIATIONS amp ALERTS Advisory Annunciations ssssssseeeennnennennennnn Comparator Annunciations
19. STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL Key on the Control Unit to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This will not delete the stored flight plan only the active flight plan sjueuinijsu fid olpny uqax u102 AEN VERTICAL NAVIGATION VNAV 52 The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually KI DFW m 25 e 221 TTE SI aroe Whi 221 9 0 12400FT d 220 80NM 9900FT Light 2 4 Approach KDFW RNAV 17Laps LPV Blue Text RIVET iof 2597 18 8NM 3 3NH Small Light Blue Tex aouepioay puezey Smai nn IE Blue Subdued 3 9NH Text d E Small White Text f 990 0 8 with Altitude 8g POLKE Restriction Bar 5 S L R Cross AT or ABOVE 5 000 fi 5 1616 ma Cross AT or BELOW 3 000 ft Facing Cross AT 2 300 fi x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 15 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional AFCS Appendix Ann
20. a check mark in the box The cursor is now 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 NEW USER WAYPOINT DEFINED BY RADIALS FROM OTHER 20 1 2 3 4 5 6 7 8 9 10 V AYPOINTS Turn the large FMS Knob on the Control Unit to select the VVPT 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 The cursor is now 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 a When a flight plan is active turning the small FMS Knob to the left will d
21. 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 32 1 2 3 4 5 6 NOTE If certain GPS parameters WAAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Press the ENT Key A list of available approaches for the destination airport is displayed 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 C90A GT 190 00664 01 Rev A A GARMIN 1 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
22. database SVS SVS DISABLED Terrain DB resolution too low Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER message Message criteria entered by the user 76 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A GARMI N LLL Appendix APPENDIX sjueuinisu iui PFD SOFTKEY MAP optional 77 rm r 7 sm umumi olpny uqax u102 AEN 52 AEN 540 Top Level PFD 50 5 optional 2 2 F EY V3 nD V3 HE S v nw D FE optional optional optional T r sem Tene es Jrennn rewec vexeao poer aac ERTS m m m r m mu uu 74 s imnp old Select the BACK Softkey to return to the top level softkeys aouepioay puezey Inset Map Softkeys m INSET Displays Inset Map in PFD lower left corner OFF Removes Inset Map gt DCLIR 3 Selects desired amount of map detail cycles 2 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 kej o s m x x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 71 Additional Hazard Flight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPD
23. 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 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 61 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx SjueuinJjsu paezey Wij w09 eN Wij SoJnjeoj Jeuonippy IUE x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix z Index Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT A G
24. gt 7 kts Differ ence in heading sensors is gt 6 degrees Differ ence in pitch sensors is gt 5 degrees Diffe ence in roll sensors is gt 6 degrees ALT NO COMP o data from one or both altitude sensors IAS NO COMP o data from one or both airspeed sensors HDG NO COMP PIT NO COMP o data from one or both heading sensors o data from one or both pitch sensors ROL NO COMP o data from one or both roll sensors 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 53 e uepioAy seinpa2o0Jd AEN 540 24V oipny uddx siu u nnsul psezeH Wij U105 AEN fij SoJnjeeoj Jeuonippy d owe x pul 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 Heading 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
25. navigate locked flight plan Comments This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at waypoint boxx Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep tum is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft will penetrate the airspace within 10 minutes ARSPC NEAR Airspace near and ahead Special use airspace is near and ahead of the aircraft position ARSPC NEAR Airspace near less than 2 nm Special use airspace is within 2 nm of the aircraft position APR INACTV Approach is not active The system notifies the pilot that the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver PTK FAIL Parallel track unavailabl
26. navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by WAAS is unavailable use LNAV only minimums Change HDG reference to TRUE TRUE APR True north approach Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 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 service Return NAV2 needs unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cyde 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 sho
27. old Strike is between 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode 1 2 With the Weather Group selected press the ENT Key The cursor flashes on STRMSCP LTNG Turn the large FMS Knob to select STRMSCP MODE 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 35 AEN Sd5 52 oipny uadx sjueumasuj U405 AEN Wij Buruue d 164 s mnp olq puezey sainjea4 leuonippy SH ly unuuy xipuaddy x pul Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Hazard Avoidance Procedures Additional Annun Alerts Features Appendix Index Hazard Avoidance GARMI N 36 3 Turn the small FMS Knob to display the Cell Strike window 4 Turn either FMS Knob to select Cell or Strike Press the ENT Key 5 Push the FMS Knob to return to the Navigation Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page 1 Tum the large FM
28. provided by the GDL 69A is approved only for weather avoidance not penetration Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN ailing Cautians amp Notes WARNING NEXRAD weather data is to be used for long range planning purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD weather data should not be used for short range weather avoidance WARNING Use of the Stormscope is not intended for hazardous weather penetration thunderstorm penetration Stormscope information as displayed on the G1000 MFD is to be used only for weather avoidance not penetration WARNING The Garmin G1000 as installed in the Hawker Beechcraft C90A GT 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 Itis thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solel
29. 0 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 83 GARMIN Appendix Slu u nnsul 1i oipny uddx wo gt AeN S24V ARN Sd5 nubi Blank Page s snp old e uepioAy paezey sainjea4 yeuonippv sH ly unuuy xipuaddy x pul Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A 84 A GARMIN A Activate a flight plan 14 Active Channel 51 ADF 5 6 80 ADS B 82 AHRS 68 69 70 72 Air Data Computer 54 Airport Signs 47 48 Airways 83 Alert messages 71 ALT 40 Altitude mode 40 Altitude volume 40 Antenna stabilization 44 Antenna tilt 43 AP 54 Attitude amp Heading Reference System 54 Audio panel controls NAV1 NAV2 6 Barometric Altitude Minimums 3 Barometric pressure 80 Bearing line 43 44 C CDI 1 2 6 74 Cell 35 36 Cell mode 36 Channel Presets 52 ChartView 48 49 Code selection softkeys 5 COM 5 6 D Database Updates 83 DCLTR Softkey 48 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT Index Declutter 77 83 Direct to 13 DME 5 6 E Edit a flight plan 28 F FD 54 Flight Director 9 Flight path marker 47 FliteCharts 48 49 Frequency Transfer 6 G Gain 44 H HF 5 6 Horizon heading 47 Horizontal scan 43 Inhibit 41 Inhibit TAWS 41 Inset Map 77 78 IOI 56 J Jeppesen 49 L Lightning 35 36 78
30. 00664 01 Rev A GARMIN 8 HilghtPlaming 6 Enter the departure time Press the ENT Key vvhen finished Departure time may be entered in local or UTC time depending upon system settings 5109 011115 7 flashing cursor moves to the ground speed GS field Enter the ground speed Press the ENT Key when finished Note that in automatic page mode ground speed is provided by the system oipny uddx u102 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 52 9 flashing 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 AUT
31. 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 Key Once all changes have been made press the FMS Knob to remove the cursor INVERT AND ACTIVATE A STORED FLIGHT PLAN 28 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 f
32. 4 01 Rev A A GARMIN 00000 Appendix MAP Enables second level Navigation Map softkeys sjueumasu 1i TRAFFIC Displays traffic information on Navigation Map TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map oipny uddx U105 AEN TERRAIN Displays terrain information on Navigation Map AIRWAYS Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON AIl airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed 52 AEN 540 STRMSCP Displays Stormscope weather and coverage information on Navigation Map optional feature NEXRAD Displays NEXRAD weather and coverage informa tion on Navigation Map optional feature Buruue d 16114 s imnp old XM LING Displays XM lightning information on Navigation Map optional feature BACK Returns to top level softkeys aouepioay puezey DCLIR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active SoJnjeoj Jeuonippy flight plan E SHW CHRT When available displays optional airport and terminal procedure charts CHKLIST When available displays optional checklists gt kej o m x x pul 19
33. 7 Weather radar 42 Wind data 80 190 00664 01 Rev A A GARMIN 00 l ndex X XM lightning 78 83 XM weather 37 XPDR Softkey 5 SoJnjeo4 eouepioAy seinpa2oJd AEN 540 52 oipny uddx Sjueuingjsu paezey Wij w09 eN Wij Jeuonippy SH ly unuuy gt 5 o 3 m x 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT ndex 3 GARMIN index Sjueuinijsu 1i oipny uddx wo gt AeN S24V ARN Sd5 Wila Blank Page sainpsr0ld eo uepioAy paezey sainjea4 SH ly unuuy xipu ddy EZ 190 00664 01 Rev A Index 4 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 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 m e 2345 Turner Road SE Salem OR 97302 U S A p 503 391 3411 f 503 364 21 Garmin Europe Ltd Liberty House Bulls Copse Roa Hounsdown Business Park Southampton SO40 9RB U K p 44 0870 8501241 f 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 www garmin com 2007 2009 Garmin Ltd or its subsidiaries 190 00664 01 Rev A
34. ARMIN 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 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 featu
35. COM2 external push to talk Switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the system should be serviced COM1 RMT XFR 1 remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck The COM1 and or COM transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its operation f the problem persists the system should be serviced LOI GPS integrity lost Crosscheck with other NAVS GPS integrity is insufficient for the current phase of flight 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 65 seinpa2oJd AEN 540 52 oipny uddx Syueuinjjsu p ezeH sufi U405 AEN sufi SoJnjeoj Jeuonippy xipuaddy x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix m Index Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message GPS NAV LOST Loss of GPS navigation Insufficient satellites Comments 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
36. 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 5 Eh ia sH ly unuuy SoJnjee4j UEP OAV s inp old Jeuonippy paezey xipuaddy x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 29 Nav Com XPDR Audio Hazard Additional Flight Instruments 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 default user waypoint naming is USR000 USR001 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 30 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 Act
37. G 1000 Integrated Flight Deck Cockpit Reference Guide for the Hawker Beechcraft C90A GT System Softvvare 0636 02 or later A GARMIN Copyright This manual reflects Beechcraf inform 91 n Ga Tel 913 397 8200 n Ga Tel 503 391 3411 m tha n Ga Sou Tel n Garmin Corporation Web Si Except as expressly p disseminated downloaded or stored en permission of Ga nd of any revision to this m writt manual a be viewed for person must contai 2007 2009 Garmin Ltd or its subsidiari t C90A GT Some differences in operation ation in this manual to earlier or later software versions International Inc 1200 East 151st Street O Vo 68 Jangsh Tel 886 02 2642 9199 te Address www garmin com n the complet es All rights reserved the operation of System Software version 0636 02 or later for the Hawker may be observed when comparing the athe Kansas 66062 U S A Fax 913 397 8282 AT Inc 2345 Turner Road SE Salem OR 97302 U S A Fax 503 364 2138 Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park mpton 5040 9RB U K 44 0870 8501241 Fax 44 0870 8501251 u 2nd Road Shiir Taipei County Taiwan Fax 886 02 2642 9099 ovided herein no part of this manual may be reproduced copied transmitted in any storage medium for any purpose without the express in hereby grants permission to download a singl
38. M Map panning 37 Message advisories 59 70 72 76 Index 1 SH ly unuuy sainjea4 aouepioay Sa1npa oJd Buruue d AEN Sd5 S24Y olpny uqax sjueumansu jeuonippy p ezeH Yu U10 AEN Wij x pu ddy Additional Hazard Flight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index MET 54 METAR 37 Minimums 57 MISCOMP 53 Mistrim 54 55 Mode S 81 Mode selection softkeys 5 Multi Function Display MFD Softkeys 82 N NACO 49 NAV 6 NAV1 2 6 NAV2 6 Navigation database 15 16 NEXRAD 37 38 78 83 0 OBS 2 Obstacles 63 65 Overspeed Protection 10 P Pathways 47 48 PIT 53 R RADIO softkey 50 ROC 55 56 S SafeTaxi 48 Sector scan 44 Sensor 54 STAB 44 Standby 42 Index 2 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT A GARMIN Store Flight Plan 27 Stormscope lightning data 35 36 78 Strike 35 Strike mode 36 SVS 47 76 SVS Terrain 47 Synthetic Vision System 47 T TA 57 TAF 37 TAS 39 40 68 TAWS 40 41 42 55 57 TAWS B 40 Terrain 40 63 78 83 Tilt line 43 Timer 73 Topographical data 78 83 Traffic 35 39 78 83 Traffic advisory 38 Traffic Advisory 57 Traffic map page 39 40 Transponder 5 81 82 V Vertical speed guidance 16 Vertical track 57 VNV 13 75 Vspeed 2 W WAAS 65 WATCH 44 Weather Attenuated Color Highlight 44 Weather data link page 3
39. Mode C Altitude Reporting Mode 22 transponder replies to identification and 8 altitude interrogations GND Manually selects Ground Mode the transponder does not allovv Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations SH ly unuuy bi kej o 3 m Ej x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 81 A GARMIN Appendix 2 3 VFR Automatically enters the VFR code 1200 in es the U S A only 2 CODE Displays transponder code selection soft keys 0 7 g 0 7 Use numbers to enter code BKSP Removes numbers entered one at a time IDENT Activates the Special Position Identification 5 SPI pulse for 18 seconds identifying the transponder return on the ATC screen ADS B TX Activates deactivates transmission of the 2 aircrafts three dimensional position and E aircraft heading for reception by ADS B systems 2 TMR REF Displays Timer References Window NRST Displays Nearest Airports Window ALERT Displays Alerts Window MFD SOFTKEY MAP 25 D w FA KES Additional Appendix Annun Alerts Features Index 82 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT Select the BACK Softkey on this level to return to the top softkey level optional optional optional ISTRMSCP NEXRAD XM LTNG BACK 7 ES v3 n MFD Softkeys 190 0066
40. Move the Joystick right or left to move the scanned slice a few degrees right or left 4 Turn the Joystick to adjust the range 5 To select a new area to be vertically scanned select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps Adjusting Gain o 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 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 43 AEN SdD S24V olpny uqax sjueumasuj u105 NeN 16114 s inp olq puezey sainjea4 jeuonippy SH ly unuuy xipuaddy x pul Hazard Avoidance GARMI N s 1 Select the GAIN Softkey to activate the cursor in the GAIN field HE 2 Turn the small FMS Knob to adjust the gain for the desirable level The gain setting is visible in the gain field as a movable horizontal bar in PE a flashing box The line pointer is a reference depicting the calibrated E position 2g 3 Press the FMS Knob to remove the cursor 4 Select the GAIN Softkey again to recalibrate the gain CALIBRATED will be 9 displayed in the GAIN field Ground Mapping gt 1 Select the MODE Softkey 5 2 Select the GROUND Softkey to place the radar in Ground Map Mode
41. OMATIC 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 e a o a m z o aouepioay puezey 13 SoJnjeej Jeuonippy CREATE A NEW 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 SH ly unuuy xipuaddy 4 Enter the desired waypoint name 5 Press the ENT Key x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 19 Nav Com XPDR Audio Hazard Additional Flight Instruments 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
42. PR 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 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 49 senpa2oJd AEN 540 241V oipny uadx SjueuinJjsu 36114 u105 NeN fil aouepioay puezey xipuaddy sH ly unuuy Fen Leri Jeuonippy x pul Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index Additional Features A 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 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
43. R Audio Instruments Appendix Index Appendix SENSOR TRAFFIC TOPO TERRAIN STRMSCP ADCI ADC2 AHRSI AHRS2 A GARMIN Displays traffic information on Inset Map Displays topographical data e g coast lines terrain rivers lakes and elevation scale on Inset Map Displays terrain information on Inset Map Press to display the Stormscope lightning data on the Inset Map within a 200 nm radius of the aircraft Displays NEXRAD weather and coverage information on Inset Map optional feature Displays XM lightning information on Inset Map optional feature optional Fs n rv Select the BACK Softkey to return to the top level softkeys Sensor Softkeys Displays softkeys for selecting the 1 and 2 AHRS and Air Data Computers Selects the 41 Air Data Computer Selects the 42 Air Data Computer Selects the 1 AHRS Selects the 22 AHRS 78 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN 000 Appendix mn uv ymummumnmmu mu sjueuinisu Aram n 7 m r A 1 a PRG NAV1 Select the BACK Softkey to return to the top level softkeys olpny uqax u102 AEN BRG GPS Y BRG26DP 52 Teersillareisill 1 FE LA 6 pers Trserl f F Ono ss S 7 7 74 cm Lorms om L 1L L lLewk ems z pese 1 TL 1L T ro J fates FE HNH 7 7 7 n onm PFD Configura
44. S Knob until the Map Page group is selected 2 Tum the small FMS Knob select the Stormscope Page Change the Stormscope Lightning Mode Between Cell and Strike 1 Select the Stormscope Page 2 Select the MODE Softkey The CELL and STRIKE Softkeys are displayed Select the CELL Softkey to display CELL data or select the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the Viewing Mode Between 360 and 120 1 Select the Stormscope Page 2 Select the VIEW Softkey The 360 and ARC Softkeys are displayed Select the 360 Softkey to display a 360 viewing area or select the ARC Softkey to display a 120 viewing area Select the CLEAR Softkey to remove all Stormscope lightning data from the display Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN XM WEATHER OPTIONAL Hazard Avoidance WARNING Use of XM weather for hazardous weather penetration is not recommended Weather information provided by XM Radio Service approved only for weather avoidance not penetration is Displaying XM Weather on the Navigation Map Page 1 2 Select the MAP Softkey Select the NEXRAD or XM LTNG Softkey to display the desired weather Select the
45. ail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams aid in following ground control instructions by accurately displaying the aircraft position on the map in relation to taxiways ramps runways terminals and services This database is updated on a 56 day cycle ChartView ChartView resembles the paper version of Jeppesen terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts FliteCharts resemble the paper version of National Aeronautical Charting Office NACO 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 A
46. akeoff 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 2 VS Key Roll Hold default ROL Vertical Speed Vs 8 VNV Key Roll Hold default ROL Vertical Path Tracking VPTH GPS zi 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 APR Key Approach VAPP Glidepath GP LOC Glideslope GS lz HDG Key Heading Select HDG Pitch Hold default PIT Valid VNV flight plan must be entered before VNV Key press activates flight director The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAVor APR Key press activates flight director m selected navigation receiver must have a valid LOC signal before BC Key press activates flight irector x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 9 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional GPS Nav AFCS Appendix Annun Alerts Features Avoidance Procedures Index A GARMIN AFCS VERTICAL MODES Vertical Mode Description Control Annunciation Holds the current aircraft pitch attitude Pitch Hold may be used to climb descend to the default PIT Selected Altitude Selected Altitude AFCS armed to capture the a
47. applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 2 3 Turn the large FMS Knob to select the WPT Page Group Turn the small FMS Knob to select the Airport Information Page 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 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Weather Data Link Page Select the available softkeys to select the desired XM weather product 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 Weather Data Link Page 1 2 3 Push in the Joystick to display the panning arrow Move the Joystick to place the panning arrow on AIRMETs TFRs METARS or SIGMETs 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 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 37 AEN Sd5 S24V oipny uadx sjueuma
48. be displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 4 Turn the large FMS Knob to highlight the desired arrival 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT Procedures 31 AEN 549 S24V oipny uadx sjuoumnasuj u105 NeN fila SoJnpa oJd su jy unuuy sainjea4 aouepioay jeuonippy paezey xipuaddy x pul 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 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
49. c Standby oipny uddx U105 AEN When the weather radar system is in the Weather or Ground Map Mode upon landing the system will automatically switch to Standby Mode Buruue g AEN Sd5 S24V 1614 s inp old gt lt s D a o sainjea4 jeuonippy su jy unuuy xipuaddy x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 45 Hazard Avoidance GARMI N Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Blank Page Procedures 2 5 22 E aq Additional Annun Alerts Features Appendix Index 46 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN ADDITIONAL FEATURES SYNTHETIC VISION Additional Features 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 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 optional enhancement to the G1000 system SVS is primarily comprised of a computer generate
50. ctivate field is highlighted 12 Press the ENT Key to activate Direct to Navigation from the PFD 1 Press the Direct to Key E on the PFD 2 Tum the large FMS Knob to place the cursor in the desired selection field GPS Navigation 3 Turn the small FMS Knob to begin selecting the desired identifier location etc oipny uddx syueumasu U10 AEN 52 s n e 4 aouepioay s inp olq Buruue d puezey Jeuonippy SH ly unuuy 36114 nb 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob to place the cursor over the ALT altitude field 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 13 xipuaddy x pul 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 of
51. d 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 Pathways Flight Path Marker Horizon Heading Marks Terrain and Obstacle Alerting Three dimensional Traffic Airport Signs e Runway Display Displaying SVS Terrain 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 Press the SYN TERR Softkey 4 Press the BACK Softkey to return to the previous page 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 4 SaJnpa oJd Buruue d AEN Sd5 ri olpny uqax s u uinnsu 16114 ul02 AEN Wila aouepioay puezey xipuaddy sH ly unuuy s m p q Jeuonippy x pul 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 th
52. dio 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 and squelch adjustment lighting the associated annunciator beneath the knob When the MAN SQ annunciatoris 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 C90A GT 190 00664 01 Rev A A GARMIN Fyodr Anio Pane PASSENGER ADDRESS PA SYSTEM A passenger address system is prov
53. e Comments AHRS1 TAS AHRS1 not receiving valid airspeed The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The system should be serviced AHRS2 TAS AHRS2 not receiving valid airspeed AHRS1 GPS AHRS1 using backup GPS source 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 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 68 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN Annunciations 8 Alerts GRS 77 MESSAGE ADVISORIES CONT Message AHRS1 GPS AHRS1 not receiving backup GPS information Comments The 1 AHRS is not receiv
54. e PRESETS Softkey to access the first five preset channels PS1 PS5 2 Select the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Selecting the MORE Softkey repeatedly cycles through the preset channels 3 Select any one of the PS1 PS15 softkeys to assign a number to the active channel 4 Select the SET Softkey on the desired channel number to save the channel as a preset Adjusting Volume Radio volume is controlled at each passenger station Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS ADVISORY ANNUNCIATIONS Annunciation Window Text AVN FAN 1 FAIL AVN FAN 2 FAIL PFD 1 FAN FAIL PFD 2 FAN FAIL MFD FAN FAIL Alerts Window Text Avionics cooling fan 1 is inoperative Avionics cooling fan 2 is inoperative PFD 1 cooling fan is inoperative PFD 2 cooling fan is inoperative MFD cooling fan is inoperative COMPARATOR ANNUNCIATIONS Comparator Window Text Condition Difference in altitude sensors is gt 200 ft f bot h airspeed sensors detect lt 35 knots this is inhibited f either airspeed sensor detects gt 35 knots and the difference in sensors is gt 10 kts 5 se f either airspeed sensor detects gt 80 knots and the difference in sors is
55. e bad geometry Bad parallel track geometry PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for parallel offset 74 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN Annunciations 8 Alerts MISCELLANEOUS MESSAGE ADVISOR ES CONT Message past IAF PTK FAIL Parallel track unavailable Comments IAF waypoint for parallel offset has been passed UNABLE V WPT Can t reach current vertical waypoint VNV Unavailable Unsupported leg type in flight plan 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 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
56. e 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 in electronic form it is still advisable to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing Selecting the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Selecting the DCLTR Softkey twice removes VOR station 48 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A GARMIN 5 Additional Features ID the VOR symbol and intersection names if within the airport plan view Selecting the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Selecting the DCLTR Softkey again cycles back to the original map det
57. e audio panel self test has detected a problem service Retum unit for repair in the unit Certain audio functions may still be GMA2 SERVICE GMA2 needs available and the audio panel may still be usable service Retum unit for repair The system should be serviced when possible GIA 63W MESSAGE ADVISORIES Message Comments GIA1 CONFIG G A1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d GIA1 CONFIG G A1 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 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 G A1 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 se
58. e copy of this anual onto a hard drive or other electronic storage medium to al use provided that such electronic or printed copy of this manual or revision e text of this copyright notice and provided further that any unauthorized rmin Garm commercial Garmin FliteChart NavData is a registered trademark of Jeppesen In Satellite Radio Inc March 2009 distribution of this man and G1000 a s and SafeTaxi are tradem not be used without the express permission of Garmin ual or any revision hereto is strictly prohibited red ts subsidiaries WATCH ies These trademarks may trademarks of Garmin Ltd or i arks of Garmin Ltd or its subsidia e registe C XM is a registered trademark of XM 190 00664 01 Rev A Printed in the U S A A Warnings Cautions amp Notes 00 GARMIN e e eo 6 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 sa
59. e flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the G1000 Pilot s Guide for this aircraft 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT A Warnings Cautions amp Notes 0 GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN YFecerdof Revisions Change Summary 190 00664 00 Initial release at GDU 8 10 190 00664 01 Added Synthetic Vision System Added GDU 9 14 parameters Revision Date of Revision Affected Pages March 2009 Production release 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT RR 1 Record ofRevisions GARMIN Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A GARMIN able of Contents FLIGHT ss ss s s 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg 1 Change Altimeter Barometric Pressure Setting Uni
60. e heard PFT Preflight system test has failed AEN Sd5 TAWS ALERTS PFD MFD Ten pl Alert Type 1 TAWS B Page Aural Message et Pop Up Alert m 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 Warning TC or 8 Terrain Ahead Pull Up Terrain Ahead Pull Up TERRAIN AHEAD PULL UP Terrain Ahead Pull Up Ter m o o o Jeuonippy Imminent Terrain PULL UP Impact Warning ITI or rain Ahead Pull Up Ns Terrain Terrain Pull Up Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Obstacle Clearance or Up Pull Up R i 3 Obstacle Ahead Pull Obstacle Ahead Pull Up x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 55 Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts A GARMIN PFD MFD MFD Alert Type 1 TAWS B Page Aural Message ave Pop Up Alert Annunciation Imminent Obstacle PULL UP Obstacle Ahead Pull Up Impact Warning or Obstacle Ahead Pull Up y Obstacle Obstacle Pull Up Pull Up Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution
61. e small FMS Knob to select Enable TAWS Press the ENT Key NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix AIRBORNE COLOR WEATHER RADAR 42 WARNING Begin transmitting only when it is safe to do so If it is desired to transmit while the aircraft is on the ground no personnel or objects should be within 11 feet of the antenna CAUTION In Standby Mode the antenna is parked at the center line It is always a good idea to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly Displaying Weather on the Weather Radar 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 Weather Radar Page Select the MODE Softkey If the aircraft is on the ground select the STANDBY Softkey to initiate the one minute warm up period After the warm up is complete the radar will enter the Standby Mode After the aircraft is airborne select the WEATHER Softkey Or If the aircraft is already airborne select the WEATHER or GROUND Softkey The one minute warm up period will be initiated after which the radar will begin
62. eference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds current aircraft roll attitude Roll Hold or rolls wings level depending default ROL on commanded bank angle Limits maximum commanded BANK R Low Bank roll angle Key Heading Select Captures and tracks Selected HDG HDG Heading Key Navigation GPS Arm Capture Track Sm Navigation VOR Enroute 1 Captures and tracks selected NAV VOR Arm Capture Track navigation source GPS VOR Key Navigation LOC Arm LOC Capture Track LOC No Glideslope Backcourse Arm Capture Captures and tracks a localizer BC Key BC Track signal for backcourse approaches Approach GPS Arm Gps Capture Track 75 mi Captures and tracks selected VAPP p navigation source GPS VOR APR Key Approach ILS Arm LOC Capture Track LOC Glideslope Mode automatically armed Disengages autopilot and Takeoff on around commands a constan pitch 10 angle and wings level in r preparation for takeoff G Switch Disengages autopilot and Go Around in air commands a constant pitch GA angle and wings level in the air No annunciation ap in the AFCS Status Box The acceptable bank angle ra green along the Ro 190 00664 01 Rev A Scale of the Attitude Indicator ge is indicated in Garmin G1000 Cockpit Reference Gu
63. esired radial from the reference waypoint 15 Press the ENT Key 16 Press the FMS Knob to remove the flashing cursor UEP OAV s imnp old paezey SoJnjee4j Jeuonippy 11 12 13 14 SS SH ly unuuy xipuaddy x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 21 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 NEW USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM 22 1 2 3 4 5 6 1 8 9 10 ANOTHER WAYPOINT Turn the large FMS Knob on the MFD Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box The cursor is now in the WAYPOINT TYPE field Turn the small FMS Knob to display a list of waypoint types Tu
64. fe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74B Air Data Computer or other altimeters in the aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on system displays is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING XM Weather should not be used for hazardous weather penetration Weather information
65. fset 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 tum the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key on the Control Unit and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 1 N 3 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint Select the ACT LEG Softkey OR Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A GARMIN GPS Navigation
66. ftkey Select the TEST Softkey Self test will take approximately eight seconds to complete When completed successfully traffic symbols will be displayed and a voice alert appropriate for the installed system will be heard indicating the test passed see Annuciations amp Alerts section If the self test fails the system will revert to Standby Mode and a voice alert appropriate for the installed system will be heard indicating the test failed 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT Hazard Avoidance AEN 540 S24V oipny uadx sjuoumnasuj u105 NeN 36114 164 puezey sainjea4 jeuonippy SH ly unuuy xipuaddy x pul 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 i
67. gt 5 Eh ti 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 desired reserve fuel quantity 6 Press the FMS Knob to remove the cursor 7 Press the ENT Key TRIP PLANNING SoJnjee4j 9 uepioAVy paezey Jeuonippy SH ly unuuy 1 Tum 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 x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 17 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning 4 For a b o d Or For a b d Or Fo a b o d A GARMIN Direct to planning Select the VVPTS Softkey and verify that the starting vvaypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to di
68. ide for the Hawker Beechcraft C90A GT 11 slu u nnsul oipny uddx U105 AEN SH ly unuuy sainjea4 aouepioay Sa1npa oJd Buruue d jeuonippy paezey xipuaddy x pul ufi AEN Sd5 S2dV nb GARMIN AFCS Slu u nnsul oE oipny YaddX wo gt AeN S24V ARN Sd5 nubi Blank Page s snp old e uepioAy paezey sainjea4 yeuonippv sH ly unuuy xipuaddy x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 12 A GARMIN GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation from the MFD 1 Press the Direct to SJ Key on the Control Unit 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 5 Turn the large FMS Knob to place the cursor over the VNV altitude field 6 Enter the desired altitude 7 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 9 8 Turn the small FMS Knob to select MSL or AGE 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 A
69. ided 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 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 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 7 sH ly
70. ight 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 partial 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 p
71. ing backup GPS information The system should be serviced AHRS2 GPS AHRS2 not receiving backup GPS information The 2 AHRS is not receiving backup GPS information The system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The system should be serviced AHRS2 GPS AHRS2 operating exclusively in no GPS mode The 2 AHRS is operating exclusively in no GPS mode The system should be serviced AHRS MAG DB AHRS magnetic model database version mismatch The 1 AHRS and 2 AHRS magnetic model database versions do not match AHRS1 SRVC AHRS1 Magnetic field model needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical AHRS2 SRVC AHRS2 Magnetic field model needs update The 2 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far North South no magnetic compass GEO LIMITS AHRS2 too far North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid 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 2 AHRS has incorrect s
72. inside this product may contain mercury Hg and must be recycled or disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp WARNING Because of anomalies in the earth s magnetic field operating the G1000 within the following areas could result in loss of reliable attitude and heading indications North of 70 North latitude and south of 70 South latitude An area north of 65 North latitude between longitude 75 West and 120 West An area south of 55 South latitude between longitude 120 East and 165 East CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings CAUTION The Garmin G1000 does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the m
73. isplay a list of the flight plan waypoints Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A GARMIN Planning b Tum the large FMS to select the desired vvaypoint Press the ENT Key sjueuinisu fid Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list 3 is displayed B b Turn the small FMS Knob to the right to display the NRST waypoints to the aircraft s current position 52 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 5 Eh 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 d
74. ive 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 C90A GT 190 00664 01 Rev A A GARMIN PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Tum the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure will be active when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the departure 4 Select the ACT LEG Softkey A confirmation window showing the selected leg will
75. keys to change how wind data is displayed 4 To remove the Wind Data Window press the OFF Softkey SoJnjeej Jeuonippy SH ly unuuy xipuaddy x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 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 C90A GT A GARMIN 190 00664 01 Rev A A GARMIN Natom APPR Andia Pane NAV COM TRANSPONDER AUDIO PANEL ADF TUNING OPTIONAL Tune the ADF using the remote ADF control head DME TUNING 1 2 3 4 Press the DME Softkey Turn the large FMS to select the DME source field Turn the small FMS Knob to select the desired Nav radio Press the ENT Key to complete the selection ENTER A TRANSPONDER CODE 1 2 3 4 Press the XPDR Softkey to display the transponder mode selection softkeys Press the XPDR1 or XPDR2 Softkey to select the active transponder Press the CODE Softkey to display the transponder code selection softkeys for digit entry Press the digit softkeys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered
76. lable gt excessively degraded GPS TANS Available E signal will be heard when sufficient GPS signal is re established System Test in progress TAWS TEST None None System Test pass None None Chime 2 AURAL ALERTS 8 Aural Alert Description 3 Minimums The aircraft has descended below the preset minimum descent altitude or 5 decision altitude Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled EE Traffic Played when a Traffic Advisory TA is issued with the TIS system s 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 12 Traffic for each subsequent TA 28 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 1 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 5KY497 TAS system passes a pilot initiated self Passed test optional Skywatch System Test Played when the optional SKY497 TAS system fails a pilot initiated self test 1 Failed optional x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 57 Hazard Flight Nav Com Fl
77. lan 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 renamed One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system Flight plan successfully exported The stored flight plan was successfully exported to the SD card Flight plan export failed The stored flight plan was not successfully exported to the SD card The SD card may not have sufficient available memory or the card may have been removed prematurely 58 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT
78. layed 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 Obstade 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 Enable TAWS While the TAWS B Page is displayed select the INHIBIT Softkey Or 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT Hazard Avoidance 41 AEN Sd5 S24V oipny uadx sjusumasuj U405 NEN Wij 164 s mnp olq puezey sainjea4 leuonippy SH ly unuuy xipuaddy x pul Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Fight Planning DEPT Avoidance Procedures Additional Appendix Annun Alerts Features Index Hazard Avoidance 1 2 3 A GARMIN While the TAWS B Page is displayed press the MENU Key Turn th
79. ltitude AUS Armed displayed in the Selected Altitude window Altitude Hold Holds the current Altitude Reference ALT Key ALT nnnnn r Maintains the current aircraft vertical Vertical Speed speed may be used to dimb descend VS Key VS nnnn rem to the Selected Altitude Flight Level Change Maintains the current aircraft airspeed Hc IAS Hold in IAS or Mach while the aircraft is id dimbing descending to the Selected FLC Key Flight Level Change Altitude Press the SPD Key to switch EC Minn Mach Hold between IAS and MACH VNAV Captures and tracks the VNAV flight VNV VPTH path Key AFCS armed to capture the altitude VNAV Target i Altitude Armed disp ayed in the VNAV Target Altitude ALTV window Glidepath Captures and tracks the WAAS GP glidepath on approach ARIA R y Glideslope Captures and tracks the ILS glideslope GS on approach Disengages the autopilot and Takeoff on ground commands a constant pitch angle and TO wings level in the air on the ground in GA preparation for takeoff dh Disengages the autopilot and Go Around in air commands a constant pitch attitude GA and wings level in the air ALTS armed automatica 10 ly when PIT VS FLC TO or GA active and under VPTH when Selected Altitude is to be captured instead of VNAV Target Altitude ALIV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude Garmin G1000 Cockpit R
80. m 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 60 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN Annunciations 8 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 error 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
81. n FPL WPT MOVE Flight plan waypoint moved TIMER EXPIRD Timer has expired The system has detected that a waypoint coordinate has changed due to a new aviation database update Verify that stored flight plans contain correct waypoint locations The system notifies the pilot that the timer has expired DB CHANGE Database changed Verify user modified procedures This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an aviation database update Verify that the user modified procedures in stored flight plans are correct and up to date DB CHANGE Database changed Verify stored airways This occurs when a stored flight plan contains an airway that is no longer consistent with the aviation database This alert is issued only after an aviation database update Verify use of airways in stored flight plans and reload airways as needed 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 13 eouepioAy seinpa2oJd AEN 540 24V oipny uddx SjueuinJjsu paezey ub U105 AEN Wij s m Jeuonippy xipuaddy x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix m Index Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message LOCKED FPL Cannot
82. ng 1 Information Window through NAVI or GPS waypoint identifier and GPS derived distance information and ADF frequency Displays the HSI formatting softkeys Displays the HSI in a 360 degree format Displays the HST in an arc format Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information and ADF frequency Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter in meters Press to display the BARO setting as inches of mercury Press to display the BARO setting as hectopacals Sets barometric pressure to 29 92 in Hg 1013 hPa 80 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN 0 HAppendix optional 7 summ us rv m sjueuinisu Ev rv ou r nn r Select the BACK Softkey to return to the top level softkeys oipny uddx u102 AEN 3IE3E IE AE Tom Tser TE Yaram EY EY EY EY 7 EN EY EY EY EY S Select the BACK Softkey to return to the previous level softkeys 52 ACN 540 Transponder Softkeys 1614 XPDR Displays transponder mode selection softkeys XPDRI Selects the 1 transponder as active 5 XPDR2 Selects the 42 transponder as active d STBY Selects Standby Mode transponder does not reply to any interrogations ir ON Selects Mode A transponder replies to a interrogations ALT Selects
83. nob to display the Categories list Highlight the desired category with the 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 Entering a Channel Directly 1 While on the XM Radio Page select the CHNL Softkey 2 Select the DIR CH Softkey The channel number in the Active Channel Box will be highlighted 3 Using the numeric keys enter the desired channel number 4 Press the ENT Key to activate the selected channel 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 5 Sa1npa oJd Buruue d AEN Sd5 24V olpny uqax s u uinnsu 16114 ul02 AEN Wila 2 xipuaddy sH ly unuuy s mn p q Jeuonippy x pul Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features GARMIN 52 Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 On the XM Radio Page with the desired channel active select th
84. oftware installed The system should be serviced 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 69 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx SjueuinJjsu psezeH Wij U405 AEN Wij SoJnjeeoj Jeuonippy 1 x pul Hazard Fight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts GMU 44 MESSAGE ADVISORIES A GARMIN Message HDG FAULT AHRS1 magnetometer fault has occurred Comments A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced HDG FAULT AHRS2 magnetometer fault has occurred A fault has occurred in the 2 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced MANIFEST GMU1 software mismatch communication halted MANIFEST GMU2 software mismatch communication halted The GMU 44 has incorrect software installed The system should be serviced GDL 69A MESSAGE ADVISORIES Message Comments GDL69 CONFIG GDL 69 config error Config service req d GDL 69 configuration settings do not match those of backup configuration memory The system should be serviced GDL69 FAIL GDL 69 has failed MANIFEST GDL software
85. og Page Select the NEW Softkey to display a blank flight plan for the first empty storage location Turn the small FMS Knob to display the Waypoint Information Window Enter the identifier of the departure waypoint Press the ENT Key Repeat step number 4 5 and 6 to enter the identifier for 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 Using the PFD 1 2 3 4 5 6 7 8 NOTE If a flight plan is active an additional flight plan cannot be entered using the PFD NOTE After the first leg is entered using the PFD only it is immediately activated Press the FPL Key on the PFD Press the FMS Knob to activate the cursor Turn the small FMS Knob to enter the first letter of the destination waypoint identifier Turn the large FMS Knob to the right to move the cursor to the next character position Repeat step 3 and 4 to spell out the rest of the waypoint identifier Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint Repeat steps 3 through 6 to enter the identifier for each additional flight plan waypoint Once all waypoints have been entered press the FMS Knob to remove the cursor The new flight plan is now active Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN
86. oint The new waypoint will be inserted before the highlighted waypoint SH ly 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 x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 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 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 Turn the large FMS Knob to select the desired waypoint d Press the ENT Key ENTER AN AIRWAY IN A FLIGHT PLAN 26 1 2 3 4 5 6 7 Press the FPL Key on the Control Unit Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint after the desired airway entr
87. or the Hawker Beechcraft C90A GT 190 00664 01 Rev A GARMIN HilghtPlaming 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 sjueumasu iui oipny uadx U105 AEN COPY A FLIGHT PLAN 52 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 15 confirmation window is displayed 6 With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN 1 Press the FPL Key on the Control Unit 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 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
88. ost current G1000 system and aviation databases Depictions of equipment may differ slightly from the actual equipment Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A 4 GARMIN amp Notes NOTE This device complies vvith part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data NOTE This product its packaging and its components 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 th
89. paration meet TA criteria Traffic Advisory Off Scale Traffic Symbol Description Traffic Information Service TIS NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS TIS is not available for use 38 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN 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 So
90. re Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced DB MISMATCH Aviation database version mismatch Xtalk is off The PFDs and MFD have different aviation database versions installed Crossfill is off Install correct aviation database version in all displays 62 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN Annunciations 8 Alerts DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Aviation database type mismatch Xtalk is off Comments The PFDs and MFD have different aviation database types installed Americas European etc Crossfill is off Install correct aviation database type in all displays DB MISMATCH Terrain database version mismatch DB MISMATCH Terrain database type mismatch The PFDs and MFD have different terrain database versions installed Install correct terrain database version in all displays The PFDs and MFD have different terrain database types installed Install correct terrain database type in all displays DB MISMATCH Obstacle database version mismatch The PFDs and MFD have different obstacle database versions installed Install correct obstacle database version in all displays DB MISMATCH Airport Terrain database mismatch The PFDs and MFD have different airport terrrain databases installed Ins
91. rn the small FMS Knob to select RAD DIS radial distance Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST waypoints 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 C90A GT 190 00664 01 Rev A GARMIN Flight Planning Or 2 a Turn the small FMS Knob to the left Initially a flight plan waypoint list E is displayed 2 b Tum the small FMS Knob to the right to display the RECENT T waypoints ES Ja Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Press the ENT Key The cursor is di
92. rviced 64 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A Annunciations 8 Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message Comments HW MISMATCH GIA hardware mismatch G A1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted A GIA mismatch has been detected where only one is WAAS capable MANIFEST G A1 software mismatch communication 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 COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM 2 over temp Reducing transmitter power The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the system should be serviced COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair 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 COMI PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The COM1 and or
93. s 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 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 40 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 TAVVS System Test OK will be heard Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN Display Terrain on the TAWS B Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAVVS B Page 3 If desired select the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is disp
94. splay P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint point to point planning Enter the identifier of the starting waypoint Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again enter the identifier of the ending waypoint Press the ENT Key to accept the waypoint flight plan leg planning 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 C90A GT 190
95. splayed in the RAD radial field Enter the desired radial from the reference waypoint 12 Press the ENT Key 13 The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 14 Press the ENT Key 15 Press the FMS Knob to remove the flashing cursor 52 AEN 540 11 Get e a o m E o puezey DELETE A USER WAYPOINT soinjes Jeuonippy 1 Tum 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 The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key SH ly unuuy xipuaddy x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 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 NEW FLIGHT PLAN Using the MFD 24 1 2 3 4 5 6 1 8 Press the FPL Key on the Control Unit Turn the small FMS Knob to display the Flight Plan Catal
96. suj U405 AEN 164 saunpar0ld puezey sainjea4 jeuonippy SH ly unuuy xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Additional AFCS GPS Nav Procedures 2 s 22 E lt x Appendix Annun Alerts Features Index Hazard Avoidance GARMI N information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information Weather Products and Symbols Echo Top Cloud Top and Echo Top Mutually Exclusive Cydone Warnings AIREP City F t Icing Potential E Cell Movement eae Freezing Levels l Turbulence PIREPs XM Lightning METARs Surface Analysis County Warnings Cloud Top SIGMET AIRMETS Winds Aloft 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 Traffic Symbol Description e 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 O Traffic Advisory TA closing rate distance and vertical se
97. tall correct airport terrain database in all displays GMA 1347D MESSAGE ADVISORIES Message Comments GMAT FAIL GMAT is inoperative GMA 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 service req d GMA2 CONFIG GMA config error Config service req d The audio panel configuration settings do not match backup configuration memory The system should be serviced 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 63 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx SjueuinJjsu paezey Wij w09 eN Wij SoJnjeoj Jeuonippy xipuaddy x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Pene Index Annunciations amp Alerts A GARMIN GMA 1347D MESSAGE ADVISORIES CONT Message Comments MANIFEST GMA1 software mismatch communication halted The audio panel has incorrect software installed The MANIFEST GMA software System should be serviced mismatch communication halted GMA1 SERVICE GMAT needs Th
98. tings 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 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 59 eouepioAy seinpa2oJd AEN 540 52 oipny uddx SjueuinJjsu paezey Wij w09 e Wij soinjes Jeuonippy id EMEN x pul 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 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 syste
99. tion Softkeys 3 PFD Displays second level softkeys for 5 2 additional configurations ge SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features SoJnjee4j Jeuonippy PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction SH ly unuuy HRZN HDG Displays compass heading along the Zero Pitch line D gt so o F m 3 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 x pul 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 79 Additional Hazard Flight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index Appendix DFLTS WIND DME BRGI HSI FRMT BRG2 ALT UNIT STD BARO OPTN 1 OPTN 2 OPTN3 OFF 360 HSI ARC HSI METERS IN HPA A GARMIN Resets PFD to default settings including changing units to standard Displays softkeys to select wind data parameters Direction arrow and numeric speed Direction arrow with numeric direction and magnitude Headwind tailwind and crosswind arrows with numeric speed components Information not displayed Displays the DME Information Window Cycles the Beari
100. transmitting The horizontal scan is initially displayed Turn the Joystick to select the desired range If desired select the VERTICAL Softkey for vertical scanning Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A GARMIN Hazard avoidance 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 Tum the large FMS Knob to select Show Tilt Line 3 Press the ENT Key Adjusting Antenna Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left Monitor the displayed bearing value in the BEARING feld When scanning horizontally a Bearing Line may be displayed to aid in positioning the antenna for the vertical scan If the Bearing Line is not displayed perform the following steps 1 Press the MENU Key 2 Tum the large FMS Knob to select Show Bearing Line 3 Press the ENT Key Vertically Scan a Storm Cell 1 While in the Horizontal Scan view move the Joystick to place the Bearing Line on the desired storm cell or other area to be vertically scanned 2 Select the VERTICAL Softkey A vertical slice of the selected area will now be displayed 3
101. ts sss 1 Synchronizing the Altimeter Barometric Pressure 1 5 1 Synchronize CDI d s n dete dee eite ed e de s s n Change Navigation Sources Enable Disable OBS Mode While Navigating with GPS 2 Generic Timer seen 2 Configure Vspeed Bugs Individually sss 2 Turn Vspeed Bugs On or Off by Category 3 Set Barometric Minimum Descent Altitude ss 3 Displaying Wind Data 3 NAV COM TRANSPONDER AUDIO PANEL 5 ADF ECOLE 5 DME Tunihj erre ree tert ae aen tartara ver ain 5 Enter a Transponder sss 5 Activate ADS B Transmit seen 5 Selecting a COM Radio 5 Selecting a NAV Radio ore ee aaro e ea a pe 6 NAV COM Tunilig ee ire e rege e iren 6 intercomo r s S M t E 6 Passenger Address PA System 7 Clearance Recorder and Player 7 AUTOMATIC FLIGHT CONTROL 5 9 Flight Director Activation sssssnnnnnnnnnnns 9 Vertical Modes nnne 0 Lateral Modes dado ER ERE ERR CER OR 1 GPS NAVIGATION acria RE an qiias ais dat ates 3 Direct to Navigation ssssssseseeen nnne 3 Activate a Stored Flight Plan
102. ttempt 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 72 Garmin 61000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT A key is stuck on the GMC 710 bezel Attempt to free the stuck key by pressing it several times The system should be serviced if the problem persists 190 00664 01 Rev A A GARMIN Annunciations 8 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 informatio
103. uld be serviced 66 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A A GARMIN Annunciations 8 Alerts GIA 63W MESSAGE ADVISORIES CONT Message G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair Comments 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 Comments GEA1 CONFIG GEAT config error Config service req d 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 GEA1 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 GTX 33 MESSAGE ADVISORIES Message Comments XPDR1 CONFIG XPDR1 config error Config service req d The transponder configuration settings do not match those of backup configuration memory The system should be serviced
104. un 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 altitudes will be displayed as small light blue text Altitudes that have been designated for use in vertical navigation may also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key The altitude is now displayed only as a reference It will not be used to give flight path vertical guidance Other displayed altitudes may change due to re calculations or rendered invalid as a result of manually changing an altitude to a non designated altitude White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by 1 Altitude has been The system cannot Small Text the system estimating the altitude of the aircraft as it passes over the navigation point This altitude is provided as a reference and is not designated to be used in determining vertical flight path guidance Altitude is not 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 entered by the pilot Altitude is designated for use in giving
105. unavailable ADC1 AS EC ADC1 airspeed error correction is unavailable correction is unavailable ADC2 AS EC ADC2 airspeed error GDC1 or GDC2 is reporting that the airspeed error correction is unavailable MANIFEST GDC1 software mismatch communication halted MANIFEST GDC2 software mismatch communication halted The GDC 74B has incorrect software installed The system should be serviced 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 71 eouepioAy seinpa2oJd AEN 540 52 siu u nnsul paezey Wij w09 eN Wi SoJnjeej Jeuonippy x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix ee 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 A
106. unuuy sainjea4 eouepioAy s anp old buluueld AEN 540 S24V olpny uqax sjueumasu Jeuonippy p ezeH u102 AEN xipuaddy x pul 16114 nubi A Nav Com XPDR Audio Panel GARMIN Flight Instruments Nav Com pol 5 c a x 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 190 00664 01 Rev A GARMI N AS 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 iui SE 52 22 pa eg ER o A NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in the following table when the flight director is not active activates the pilot side flight director in the listed modes AEN Sd5 Modes Selected Control Pressed 7 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 T
107. 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 use this altitude in determining vertical flight path guidance The system cannot use this altitude in determining vertical flight path guidance 16 Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT 190 00664 01 Rev A GARMI N 8 3 HightPlaming FLIGHT PLANNING sjueuinisu fid 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 52 AEN 540 zn
108. y 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 C90A GT 190 00664 01 Rev A 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 a ga c ERG oF FA i TURN VSPEED BUGS ON OR OFF BY CATEGORY oipny uddx u102 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 52 SET BAROMETRIC MINIMUM DESCENT ALTITUDE AEN Sd5 1 Press the TMR REF Softkey 2 Turn the large FMS Knob to highlight the OFF BARO field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to BARO 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 To remove the window press the CLR Key or the TMR REF Softkey seinpa2oJd Buruue d 164 puezey DISPLAYING WIND DATA 1 Press the PFD Softkey 2 Press the WIND Softkey to display wind data below the Selected Heading 3 Press one of the OPTN soft
109. y 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 C90A GT 190 00664 01 Rev A GARMIN Planning INVERT AN ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 Press the MENU Key to display the Page Menu 3 Turn the large FMS Knob to highlight Invert Flight Plan 4 Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location 5 With OK highlighted press the ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM
110. y responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the G1000 Integrated Avionics System and GFC 700 AFCS in Hawker Beechcraft C90A GT Airplane Flight Manual Supplement Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G1000 to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation 190 00664 01 Rev A Garmin G1000 Cockpit Reference Guide for the Hawker Beechcraft C90A GT A Warnings Cautions amp Notes 000 GARMIN WARNING The illustrations in this guide are only examples Never use the G1000 to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo WARNING Lamp s

Garmin Software Version 0636.02 Cockpit Reference Guide

Contents

Download Pdf Manuals

Related Search

Related Contents