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Garmin 407GX Cockpit Reference Guide

1. 1 Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 2 3 4 On the XM Radio Page while listening to an Active Channel that is wanted for a preset press the PRESETS Softkey to access the first five preset channels PS1 PS5 Press the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Pressing the MORE Softkey repeatedly cycles through the preset channels Press the SET Softkey Press any one of the PS1 PS15 softkeys to assign a number to the active channel Adjusting Volume 1 2 3 4 On the XM Radio Page press the RADIO Softkey Press the VOL Softkey to access the volume control softkeys Press VOL or VOL softkeys to adjust the volume level Press the MUTE Softkey to mute the radio audio AUXILIARY VIDEO OPTIONAL Display Auxiliary Video 1 2 Turn the large FMS Knob to select the AUX page group Turn the small FMS Knob to select VIDEO and display the AUX VIDEO Page Adjusting Video Settings 1 2 3 4 5 With the AUX VIDEO Page displayed press the SETUP Softkey Press the BRIGHT or BRIGHT to adjust display brightness in five percent increments from 0 to 10096 Press the CNTRST or CNTRST to adjust display contrast in five percent increments from 0 to 10096 Press the SAT or SAT to adjust display saturationin five percent incr
2. 112 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN GIA 63H MESSAGE ADVISORIES CONT Annunciations amp Alerts Message COMI PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck Comments The COM and o Switch is stuck in position Press th operation If the problem pe serviced COM2 external push to talk the enable or pressed e PTT switch again to cycle its sists the system should be COM1 RMT XFR 1 remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck The COM1 and or in the enabled o transfer 2 transfer switch is stuck pressed position Press the switch again to cycle its operation If the problem persists the system should be serviced LOI GPS integrity lost Crosscheck with other NAVS GPS integrity is in of flight sufficient for the current phase GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigati satellites on due to insuf f icient GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS nav
3. encre ani wien ube tl ct i ea 04 HTAWS System Status Annunciations ssssssse 05 Voice Alerts 06 MFD amp PFD Message Advisories sss 07 Database Message Advisories 08 GMA 350H Message Advisories 0 GIA 63H Message AdVISOFI6S ia 1 GEA 71H Message Advisories sssssssseee e 4 GTX 33H Message Advisories 4 GRS 77H Message Advisories 5 GMU 44 Message Advisories 5 GSR 56H Message Advisories 6 601 59H Message Advisories 6 GDL 69AH Message Advisories 6 GDC 74H Message Advisories sssssssssee 7 GTS 800 Message Advisories s s aa 7 Miscellaneous Message Advisories 7 Flight Plan Import Export Messages 21 ii 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Table of Contents GARMI N Du 22 17 PCM TTE 123 PFD Softkey Map 123 MED Softkey 129 Loading Updated Databases 131 ID C Index 1 N Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GA
4. not securely latched GT is in exceedance GT miscompare event Engine Ng is in exceedance g miscompare event Engine NP is in exceedance P miscompare event R miscompare event Pedal stop check or failed to engage or disengage upon command Or loss of ADC inputs Engine torque is in exceedance Q miscompare event Right fuel boost pump has failed Right fuel transfer pump has failed TIR Chip Detector has detected debris Transmission Chip Detector has detected debris in transmission oil Single Ping Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN ADVISORY MESSAGES See the Rotorcraft Flight Manual RFM for recommended pilot actions Annunciation Text Annunciations 8 Alerts Description ALTN DATA FAIL AUTO RELIGHT ine igniter is operating nate engine data source is not available ENG ANTI ICE 2 D Anti Ice valve is open pressure is high FADEC MAINT amp test failure during power up self test and in flight INSTR FAN C ument panel area fan has failed NG OAT LIMIT ine Ng limited due to OAT QUIET MODE SEL Quiet Mode switch is in quiet position RESTART FAULT fault will not allow start in AUTO ECU Mode START ine starter is engaged SAFE OPERATING ANNUNCIATION Annunc
5. 105 Garmin G1000H Cockpit Reference Guide for the Bell 407GX sainjea4 2 buluueld AEN Sd5 S24JV olpny uqax sv l4 sjuauimasu 2 nubi swop AeNn Yid jeuonippy uoneiedo jJeuuouqv x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Annunciations GARMIN Alert Type PFD HTAWS Page Status Annunciation HTAWS Page Center Aural Banner Annunciation Message Excessively degraded GPS signal HTAWS N A None HTAV Not Available HTAWS Available when sufficient GPS signal is received and HTAWS is not inhibited Out of database coverage area HTAWS N A None HTAV Not Available HTAWS Available when aircraft enters database coverage area and HTAWS is not inhibted Aural message not issued if HTAWS is inhibited VOICE ALERTS Voice Alert Minimums minimums Description he aircraft has descended below the preset barometric minimum Vertical track he aircraft is one minute from Top of Descent Issued only when 1 descent altitude 1 vertical navigation is enabled Twelve o clock or No Bearing Traffic Played when a Traffic Advisory TA is issued TIS and GTS 800 TIS Not Available The aircraft is outside the
6. Duruue d u u s mp oold paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN XM Weather Product GFDS Worldwide Weather Product XM Lightning GFDS Lightning XM LTNG DL LTNG SIGMETs AIRMETs SIGMETs AIRMETs SIG AIR SIG AIR Meteorological Aerodrome Report METARs Meteorological Aerodrome Report METARs Winds Aloft WIND Pilot Weather Report PIREPs Winds Aloft WIND Pilot Weather Report PIREPs Restoring Default GFDS Weather Data Link Page Settings Select the GFDS Weather Data Link Page 1 2 3 4 5 Press the MENU Key With Weather Setup highlighted press the ENT Key Press the MENU Key Highlight the desired default s to restore all or for selection and press ENT Key Switching Between GFDS and XM Weather Sources 1 2 3 4 Turn the large FMS Knob on the MFD to select the MAP page group Turn the small FMS Knob to select the GFDS or XM Weather Data Link Page Press the MENU Key Turn the large FMS Knob to select Display GFDS Weather or Display XM Weather choice dependent on current weather source and press the ENT Key Viewing Le
7. Comments The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press D NAV2 RMT XFR NAV2 remote transfer key is stuck the transfer switch again to cycle its operation If the problem persists the system should be serviced G S1 FAIL G S1 is inoperative A failure has been detected in glideslope G S2 FAIL G S2 is inoperative receiver 1 and or receiver 2 The system should be serviced G S1 SERVICE G S1 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may G S2 SERVICE G S2 needs service Return unit for repair still be available The system should be serviced when possible GEA 71H MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEA1 config error Config service req d MANIFEST GEA1 software mismatch communication halted The GEA1 configuration settings do not match those of backup configuration memory The G1000H system should be serviced The 1 GEA 71 has incorrect software installed The G1000H system should be serviced GTX 33H 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 MANIFEST GTX1 software mismatch communication halted
8. In Copilot Isolate mode the Pilot Copilot and Passengers hear the aircraft audio The Pilot and Passengers also hear each other The Copilot has the option to use Split COM mode Aircraft Audio on ICS Keys Mode Operation All Isolate Mode In All Isolate mode the Pilot and Copilot hear the aircraft audio The Copilot has the option to use Split COM mode The Passengers hear each other Aircraft Audio ICS Keys Mode Operation 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 17 Sjueuinijsu wp 52 oipny uddx 597213 WOJ ABN Suelv uoneiado saunyea4 aoueplony saunpa20Jd Fuluueld AEN Sd5 unuuy jeuuouqy jeuonippy 2 wd xipuaddy x pul Flight Instruments Nav Com AFCS XPDR Audio EICAS Annun Abnormal Additional Hazard Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav Appendix Index A Nav Com XPDR Audio Panel GARMIN Pilot amp Copilot Isolate Mode In Pilot amp Copilot Isolate mode the Pilot Copilot and Passengers hear the aircraft audio The Passengers hear each other The Copilot has the option to use Split COM mode Aircraft Audio ICS Keys Mode Operation Pilot amp Passenger Isolate Mode In Pilot amp Passenger Isolate mode the Pilot and Copilot hear the aircraft audio The Passengers hear each other Aircraft Audio ICS Keys Mode Operation Copilot amp Passenger Isolate Mode
9. MCP shown with a red tick mark Operating limits are displayed along the PSI gauge and are calculated dynamically in response to all parameters to show the range of needle movement available beyond MCP before any parameter reaches the operating limit Green arcs indicate continuous operation ranges yellow arcs indicate transient operating limits A gray arc becomes red if the Power Available Indicator enters this range it indicates an exceedance is occurring During engine start a red triangle appears on the PSI arc when MGT is shown to correspond with MGT starting limits and remains displayed until the starter has been disengaged for 5 seconds Takeoff Timer After the engine has been started if Q or MGT are within the takeoff limitation ranges the G1000H displays a 5 minute countdown timer inside the PSI gauge The 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 7 Sjueuinijsu nubi SE xipueddy Suelv uoneiado SoJnjeaJ aoueplony saunpa20Jd Fuluueld AEN Sd5 241V olpny uqax unuuy jeuuouqy jeuonippy paezey wd U105 AEN x pul Flight Instruments EICAS Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS Procedures GPS Nav Appendix Alerts Operation Features Index 4 Engine Indication amp Crew Alerting yal GARMIN timer flashes beginning when 30 seconds remain until an exceedance will occur the timer is automatically removed
10. TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD RAD radial radial Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN Fight Planning 11 12 13 14 15 16 a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position 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
11. The transponder has incorrect software installed The system should be serviced XPDR1 SRVC XPDR1 needs service Return unit for repair The 1 transponder should be serviced when possible XPDR1 FAIL 1 is inoperative There is no communication with the 1 transponder 114 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN GRS 77H MESSAGE ADVISORIES Annunciations amp Alerts Message AHRS1 TAS AHRS1 not receiving airspeed Comments The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The system should be serviced AHRS1 GPS AHRS1 using backup GPS source The 1 AHRS is using the backup GPS path Primary GPS path has failed The system should be serviced when possible 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 AHRS1 GPS AHRS1 not receiving backup GPS information The 1 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 AHRS MAG DB AHRS magnetic model database version mismatch The 1 AHRS a
12. sjuaumasu sub PFD SOFTKEY MAP 5721 optional Es ier e s 1E 99 3 r r m rs r r m r olpny uqax U105 AeN CD NAVI A m S Top Level PFD Softkeys optional Esas pwser rs s L eor Jp owe re en ST es LA FE V3 V3 73 7 75 75 930 optional optional optional optional 3 OFF DCLTR WXLGND TRAFFIC TOPO NEXRAD XM LTNG METAR BACK MSG 2a orr lvxtssol raarric Toro mne veran T sack vec FS F3 F3 V x nnn n Press the BACK Softkey to return to 5 ze the top level softkeys B zm Gh LJ 8 gs Inset Map Softkeys 28 uoneiedo Jeuuouqy Level 1 Level 2 Level 3 Description CAS Displays the scroll up and scroll down softkeys when the number of CAS messages exceeds the maximum capable of being displayed in the window 2E ID W as 3 CAS T Moves the cursor up through the displayed d messages i CAS Y Moves the cursor down through the x pul displayed messages 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS KPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix A GARMIN Appendix Level 1 Level 2 Level 3 Description INSET Displays Inset Map in PFD lower left corner OFF Removes Inset Ma
13. A GARMIN Nav Com XPDR Audio Panel INTERCOM MODES NOTE When in Split COM mode the copilot will only hear alerts and the higher numbered of the two selected COMs COM2 or COM3 All Intercom Mode In All Intercom mode the Pilot Copilot and Passengers hear each other and hear the aircraft audio Aircraft Audio ICS Keys Mode Operation 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Sjueuinijsu sub 52 oipny uadx 5721 U105 AEN Suelv uoneiado SoJnjeaJ aoueplony saunpa20Jd Fuluueld AEN Sd5 unuuy jeuuouqy jeuonippy paezey wd xipuaddy x pul A Nav Com XPDR Audio Panel GARMIN Pilot Isolate Mode In Pilot Isolate mode the Pilot Copilot and Passengers hear the aircraft audio The Copilot and Passengers also hear each other Flight Instruments Aircraft Audio EICAS Nav Com 2 Ei x 3 2 x AFCS GPS Nav Flight Planning ICS Keys Mode Operation Procedures Passenger Crew Isolate Mode In Passenger Crew Isolate mode the Pilot and Copilot hear the aircraft audio and each other The Passengers hear each other Hazard Avoidance Aircraft Audio Additional Features Abnormal Operation ICS Keys Mode Operation Annun Appendix Alerts Index Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Nav Com XPDR Audio Panel Copilot Isolate Mode
14. In Copilot amp Passenger Isolate mode the Pilot and Copilot can hear the aircraft audio The Copilot has the option to use Split COM mode The Passengers hear each other Aircraft Audio ICS Keys Mode Operation Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Nav Com XPDR Audio Panel Blue Select Mode Telephone Entertainment Distribution The music MUSIC and telephone entertainment JA audio are distributed using the Blue Select Mode The following example indicates that the pilot copilot and passengers will all hear the telephone entertainment audio Blue Select Mode Telephone Entertainment Distribution The Blue Select Mode is entered by pressing the small knob when the the volume control cursor flashing green annunciator is not active If the voume control cursor is active press the small knob twice The first press will cancel the volume control cursor the second will activate Blue Select Mode The annunciator over the Button will be flashing blue Any combination of the annunciators over the PILOT COPLT and PASS buttons may be blue Select the desired button to turn the blue annunciator on or off to distribute the telephone audio to selected crew passenger positions Turn the large knob to select MUSIC and select the crew passenger positions to receive the music audio Selecting any button other than PILOT COPLT PASS MUSIC or will cancel Blue
15. Monitor mute enabled COM reception Disable monitored COM mute di Disables Monitored COM mute disable monitored l COM mute Voice Response Disable mute monitored COM 0 Primary Monitor mute disabled COM or 222 reception ute monitored COM disable 23 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning Nav Com AFCS XPDR Audio EICAS GPS Nav Procedures Appendix Alerts Operation Features Index Nav Com XPDR Audio Panel A GARMIN Control Spoken Command Action Confirmation of Action u Toggles Illuminate Extinguish NAV1 MANUS NAV1 Annunciator id Toggl Illuminate Extinguish NAV2 i 7 oggles uminate Extinguis MANI NAV2 Annunciator AUX ingui AUX 77 d Toggles AUX lluminate Extinguish AUX Auxiliary Annunciator Telephone or Toggles Phone or Telephone Il uminate Extinguish lack Jack Annunciator Telephone mute or Phone mute or Mutes Jack mute or Telephone Voice Response Mute telephone or Jack on radio Tel and jack mute enabled Mute phone or reception Mute jack Disable telephone mute or l Disable phone mute or Disables Disable jack mute or pu 7 Voice Response Telephone mute disable or oteli Tel and jack mute disabled Phone mute disable or reception Jack mute
16. REGISTER will now be highlighted 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 7 2 Puluueld AeN Sd5 S24V oipny uadx svola s u u nnsul nubi Tu102 AEN 346 2 xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN 10 11 12 13 Press the ENT Key System registration is complete when REGISTERED is displayed in the STATUS field Enter the last four digits of the System ID number in the Access Code field Press the ENT Key REGISTER will now be highlighted Press the ENT Key System registration is complete when REGISTERED is displayed in the STATUS field Disable Enable Iridium Transceiver Iridium telephone and data communications may be turned on or off by performing these simple steps Disabling enabling telephone and low speed data services 1 2 3 4 5 6 1 Turn the large FMS Knob on the MFD to select the AUX page group Turn the small FMS Knob to select REPORTS DATA LINK If necessary select the REPORTS Softkey The AUX REPORT STATUS Page is now displayed Press the MENU Key The Page Menu window is now displayed Turn the FMS Knob to select Disable Iridi
17. When the entry is complete press the ENT Key Turn the large FMS Knob or press the ENT Key until SAVE is highlighted Press the ENT Key Disconnecting a Wi Fi Network Press the DISCNCT Softkey Deleting a Saved Wi Fi Network 1 2 3 While viewing the list of saved networks press the FMS Knob to activate the cursor Turn either FMS Knob to highlight the network to be deleted Press the DELETE Softkey The selected network is removed from the list Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Additional Features SYSTEM DATA LOGGING OPTIONAL NOTE An account must be established vvith Garmin Flight Data Services to make full use of the System Data Logging feature Control and monitoring of report transmissions is accomplished through the AUX REPORT STATUS Page Viewing the Report Status Page 1 Turn the large FMS Knob on the MFD to select the AUX page group 2 Turn the small FMS Knob to select REPORTS DATA LINK 3 If necessary press the REPORT Softkey to display the AUX REPORT STATUS Page Changing the Transmission Method 1 While viewing the Report Status Page press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to move the cursor to the 1st or 2nd transmit method for the desired data report 3 Turn the small FMS Knob to select the desired option SAT SHORT BURST SAT RUDICS WI FI or NONE Sat Short Burst is generally used for t
18. XPDR Audio EE Abnormal Additional Hazard Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index A Procedures GARMIN 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 52 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 is displayed With ACTIVATE highlighted press the ENT Key Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN H zadavoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page XM WX SATELLITE WEATHER OPTIONAL WARNING Use of XM WX Satellite Weather for hazardous weather penetration is not recommended Weather information provide
19. svol4 siu umnisul sub oipny uadx 0105 AEN ARN Sd5 52 suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d Tunuuy Jeuuouqy Jeuonippy paezey nu xipuaddy x pul GARMIN AFCS Sjueuinijsu fila 5729 U105 AEN 52 AeN 5492 Buluuejd r Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 4076X 30 A GARMIN GPS Navigation GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation from the MFD 1 Press the Direct to E Key 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 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 Tum the small FMS Knob to select MSL or AGE 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field 10 Enter the desired offset distance before the waypoint 11 Press the ENT Key The Activate field is h
20. 15 Min 20 Min 25 Min 30 Min 45 Min or 60 Min then press the ENT Key Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN Hazard avoidance 6 The SEND REQ button is highlighted and a countdown timer is displayed in the REQUEST STATUS based on the currently selected update rate Press the ENT Key to immediately send an immediate GFDS Data Request Or Press the FMS Knob to return to the GFDS Weather Data Link Page Worldwide Weather Products Precipitation NOTE Precipitation data cannot be displayed at the same time as terrain Precipitation data is not real time The lapsed time betvveen collection processing and dissemination of radar images can be significant and may not reflect the current radar synopsis Due to the inherent delays and the relative age of the data it should be used for long range planning purposes only DISPLAYING PRECIPITATION WEATHER INFORMATION 1 Select the MAP Softkey for the PFD Inset Map select the INSET Softkey This step is not necessary on the GFDS Weather Data Link Page 2 Select the PRECIP Softkey Radar data shown represents lowest level base reflectivity of radar returns The display of the information is color coded to indicate the weather severity level All weather product legends can be viewed on the GFDS Weather Data Link Page For the Precipitation legend select the LEGEND Softkey when Precipitation is selected for displ
21. 190 01254 00 Rev B GARMIN Table of Contents FLIGHT INSTRUMENTS 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg 1 Change Altimeter Barometric Pressure Setting 5 1 Change Navigation Sources arent arenan arrra ar errant enaar 1 Enable Disable OBS Mode While Navigating with 6 5 2 Enable heading Preset Mode 2 Disable heading Preset senes 2 Generic TIMEN oe oou rct RO RR ORE dn ede 3 Configure Vspeed Bugs Individually sss 3 Set Barometric Minimum Descent Altitude sss 3 Set Barometric Radar Altimeter RA Optional Minimum Descent Altitude 4 Displaying Wind Data 4 Changing HSI FOTMAt wwwww aterra aterra atrrrn aterra arrra arenan 4 ENGINE INDICATION SYSTEM 5 Engine Power and Speed IndicatioNS ww nr 7 Power Assurance Check 8 CREW ALERTING SYSTEM CAS 9 CAS Message Prioritization 0 NAV COM TRANSPONDER AUDIO PANEL ADF Tuning Optional ssseeennntnnnntnn DME Tuning O
22. GARMIN Traffic Information Service TIS NOTE If the G1000H is configured to use a Traffic Advisory System TAS TIS is not available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page 1 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page Press the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Press the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Press 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 press the MAP Softkey Press the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory System TAS Optional NOTE Radar altimeter data is optional for the Traffic Advisory System TAS If radar altimeter data is detected by the TAS at the beginning of a power cycle and that data is subsequently lost the TAS will declare a fault and will not provide traffic information Displaying Traffic on the Traf
23. Hazard Avoidance D spLAYING SIGMETs and AIRMETs 1 Select the GFDS VVeather Data Link Page 2 select the SIG AIR Softkey 3 To view the text of the SIGMET or AIRMET press the RANGE Knob and move the Map Pointer over the icon 4 Press the ENT key To display the SIGMET and AIRMET legend select the LEGEND Softkey when SIGMETs and AIRMETs are selected for display METARs and TAFs NOTE METAR information is only displayed within the installed navigation database service area METAR and TAF text are displayed on the Weather Information Page TAF information is displayed in its raw form when it is available DisPLaviNG METAR and TAF TEXT 1 On the GFDS Weather Data Link Page select the METAR Softkey 2 Press the RANGE Knob and pan to the desired airport 3 Press the ENT Key The Weather Information Page is shown with METAR and TAF text 4 Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text METAR text must be completely scrolled through before scrolling through the TAF text 5 Press the FMS Knob or the CLR Key to return to the GFDS Weather Data Link Page Or 1 Select the Weather Information Page a Turn the large FMS Knob to select the Waypoint Page Group b Select the WX Softkey to select the Weather Information Page 2 Press the FMS Knob to display the cursor 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 65 AEN Sd 52 oipny ud
24. Key Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Or Flight Planning a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints 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 11 Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint 12 Press the ENT Key 13 The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 14 Press the ENT Key 15 Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 4 Turnthe large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn the small FMS Knob to highlight the desired waypoint 6 Press the DELETE Softkey 7 Themessage Would you like to delete the user waypoint is displa
25. Minimums 106 Mode S 128 Mode selection softkeys 11 Multi Function Display MFD Softkeys 129 N NAV 12 13 NAV1 1 NAV1 audio 13 NAV2 1 NAV2 audio 13 Navigation database 33 34 Navigation mode selection 12 Network 89 90 NEXRAD 53 124 130 NEXRAD Softkey 63 0 OBS 2 Obstacles 110 112 Oil Temperature OIL F 6 Index 2 Garmin G1000H Cockpit Reference Guide for the Bell 407GX A GARMIN P Pathways 73 74 PIREP 66 Predefined message 84 R Register 77 78 Reversionary mode 97 ROC 104 S Safelaxi 74 SBAS 50 99 112 113 Standby frequency field 11 Standby Navigation Database 133 Store Flight Plan 45 SVS 73 120 Synchronization 131 SYNC Status 134 Synthetic Vision System 73 System ID 77 78 T TA 106 TAF 53 65 TAS 68 69 106 115 Telephone 78 Terrain 70 110 124 129 Text message 82 84 85 Text messaging 81 Timer 117 Topographical data 124 129 Traffic 53 68 124 129 Traffic Advisory 106 Traffic advisory 68 Traffic map page 68 69 Transponder 11 127 128 190 01254 00 Rev B A GARMIN V Vertical speed guidance 34 Vertical track 106 VNV 31 98 119 Voice Recognition 22 VOR selection 12 Vspeed 3 W Waypoint Selection Submenu 42 Weather data link page 53 Wi Fi 89 90 91 Wind data 126 Winds Aloft 66 WIND Softkey 67 X XM lightning 124 130 XM weather 53 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bel
26. Select Mode Pressing the small knob will also cancel Blue Select Mode After approximately ten seconds with no input the Blue Select Mode will automatically cancel PASSENGER ADDRESS MODE PA MODE Press and hold the SPKR Key for 2 seconds to initiate Passenger Address Mode PA Mode is annunciated by a rapid blinking of the SPKR annunciator When in PA Mode the crew can use the PTT Push to Talk button to deliver announcements over the speaker to the passenger headsets or both depending on configuration 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Sjueuinajsu 52 oipny uddx 597213 wio gt AeN sH ly uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld AEN Sd5 unuuy jeuuouqy jeuonippy paezey Wia x pu ddy x pul fila Abnormal Additional Hazard Annun Flight Instruments Flight Planning Nav Com AFCS XPDR Audio EICAS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN SPLIT PA MODE During Split PA Mode the pilot can continue to use the radio s while the copilot delivers PA announcements To initiate Split PA Mode first enter Split COM Mode by pressing more that one MIC Keys simultaneously then press and hold the SPKR Key for 2 seconds 3D AUDIO 3D Audio is useful when multiple audio sources are present By using different responses in each ear 3D audio processing creates the illusion that each audio so
27. The altitude selection is shown at the bottom WORLDWIDE WEATHER NOTE Garmin Flight Data Services Worldwide Weather provides information for avoiding hazardous weather Do not utilize Worldwide Weather informa tion to penetrate hazardous weather Weather data are provided when the pilot initiates either a manual or automatic GFDS data request on the GFDS Weather Data Link Page on the MFD No weather data is displayed until the first GFDS Weather Data Request is made Accessing GFDS Worldwide Weather Products 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the GFDS Weather Data Link Page 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 55 AEN 549 S24V oipny uadx 5729 siu uninsul u102 AEN 1014 Duruue d nubi s mp oold paezey sualy uoneJado saunjeaj junuuy jeuuouqy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance GARMIN When a weather product is selected for display on the GFDS Weather Data Link Page a box containing a symbol for the product and its age in minutes are shown in the upper right If weather data has not been requested N A is shown next to the product symbol instead of age The age
28. Unsupported leg type in flight plan The lateral flight plan con tains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint guidance to the active ve This prevents vertical tical waypoint VNV Unavailable Excessive crosstrack error The cur vertical deviation to go in rent crosstrack exceeds the limit causing valid VNV Unavailable Parallel course selected A parallel course has bee n selected causing the vertical deviation to go in valid TRAFFIC FAIL Traffic device has failed traffic system The traffic d The system is no longer receiving data 4 rom the evice should be serviced NO WGS84 WPT Non waypoint for navigation WGS 84 f Cc a s displayed Do not use n The position of the selected waypoint xxxx s not calculated based on the WGS84 map eference datum and may be positioned in error GPS to navigate to the elected non WGS84 waypoint 190 01254 00 Rev B 119 Garmin G1000H Cockpit Reference Guide for the Bell 407GX saunjeaj s mp oold Buruue d AEN Sd5 2 oipny uddx sv l3 sjueumasu paezey nubi Juo eN Wil jeuonippy uoneiedo Jeuuouqy EET x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operatio
29. addressed Mode S interrogations Automatically enters the VFR code 1200 in the U S A only Displays transponder code selection softkeys 0 7 Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Use numbers to enter code Removes numbers entered one at a time Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Displays Timer References VVindovv Displays Nearest Airports VVindovv Displays Messages VVindovv Garmin G1000H Cockpit Reference Guide for the Bell 4076X 190 01254 00 Rev B A GARMIN Appendix MFD SOFTKEY MAP optional optional ENGINE Lier peus SHW CHRT chkust sjuauimasu Yid 5721 DCLTR 2 ence cast cas PWR CHK F3 V3 V3 F3 Press the BACK Softkey on this level to return to the top optional optional softkey level DCLTR 3 IG or optional optional olpny uqax 0105 AEN TRAFFIC ARways 4 NEXRAD XM LTNG METAR LEGEND BACK ma 7 V3 V3 VS AIRWY ON Softkeys 8 Level 1 Level 2 Level 3 Description 54 ENGINE Displays the EIS Engine Page CAS 1 Scroll up Displayed only when a SoJnpa20Jd sufficient number of items are dis
30. and obstacles that pose a threat to the aircraft in flight are shaded yellow or red In addition to SVS enhancement to the PFD the following feature enhancements have been added to the PFD e Pathways e Flight Path Marker e Horizon Heading Marks e 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 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX n 2 Buruuejd AeN Sd5 S24V oipny uadx svola s u u nnsul Tu102 AEN 346 eouepioAy paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A GARMIN Displaying Pathways 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the PATHWAY Softkey 5 Press the BACK Softkey to return to the previous page Displaying Heading on the Horizon 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey t
31. be serviced A failure has been detected in the GDL 69AH The receiver is unavailable The G1000H system should be serviced MANIFEST GDL software mismatch communication halted Garmin G1000H Cockpit Reference Guide for the Bell 407GX The GDL 69AH has incorrect software installed The G1000H system should be serviced 190 01254 00 Rev B A GARMIN GDC 74H MESSAGE ADVISORIES Annunciations amp Alerts Message MANIFEST GDC1 software mismatch communication halted Comments The GDC 74H has incorrect software installed The G1000H system should be serviced GTS 800 MESSAGE ADVISORIES Message Comments GTS CONFIG GTS config error Config service req d The GTS and GDU have incompatible configurations This alert is also set when the GTS has an invalid mode S address configured or the mode address does not match both XPDR mode addresses MANIFEST GTS software mismatch communication halted The GTS has incorrect software installed The G1000H system should be serviced MISCELLANEOUS MESSAGE ADVISORIES Message Comments FPL WPT LOCK Flight plan waypoint is locked Upon power up the system detects that a stored flight plan waypoint is locked This occurs when an navigation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur
32. disable MUSIC Toggles llluminate Extinguish MUSIC MUSIC Annunciator Mutes MUSIC mute or MUSIC Voice Response MUSIC Mute MUSIC on radio Music mute enabled reception Disables Disable MUSIC mute or MUSIC mute Voice Response MUSIC mute disable on radio Music mute disabled reception Speaker Sneaker Toggles lluminate Extinguish SPKR SPKR P SPKR on off Annunciator ip AE Toggles PA SPKR Annunciator blinks in d P on off PA mode 24 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Nav Com XPDR Audio Panel Control Spoken Command Action Confirmation of Action pilot Toggles luminate Extinguish PILOT PILOT button Annunciator Toggles T Copilot COPIT Illum nate Extinguish COPLT Annunciator button Passenger or Toggles luminate Extinguish PASS Pass PASS button Annunciator Passenger mute or Mutes Pass mute or passengers Voice Response ICS Isolation Mute passenger or during radio Passenger mute enabled Mute pass reception Disable passenger mute or Disable pass mute or Disable mute passenger or 5 Disable mute pass or muting o Voice Response Passenger mute disable or 27 Passenger mute disabled 9 during radio 9 Pass mute disable or reception Mute passenger disable or Mute pass disable Copilot is passenger or Voice Response Copilot is pass Copilot is p
33. of the weather product is based on the time difference between when the data was assembled on the ground and the current GPS time Weather products are updated continuously or refreshed at specific intervals defined in the Refresh Rate column in the following table If for any reason a weather product is not refreshed within the defined Expiration Time intervals the data is considered expired and is removed from the display The age of the expired product is replaced by dashes If more than half of the expiration time has elapsed the color of the product age readout changes to yellow The refresh rate represents the interval at which the GFDS servers make available the most current known weather data It does not necessarily represent the rate at which new content is received from weather sources Expiration Weather Product Symbol Time Minutes Radar Precipitation E 30 U S Canada 3 PRECIP Europe 15 Infrared Satellite afi IR SAT aii Datalink Lightning Er DL LTNG 30 Continuous SIGMETS AIRMETs SIDMET SIG AIR AIRMET Meteorological Aerodrome Report LE METARs T 90 Continuous Winds Aloft WIND 60 Continuous Pilot Weather Report B PIREP 90 Continuous Tam para Pigot RGSITIBIS no product image 60 Continuous TFRs 56 Garmin G1000H Cockpit Reference Guide for the Bell 4076X 190 01254 00 Rev B A GARMIN Hazard Avoidance Expirat
34. press the MAP Softkey 3 Press the TRAFFIC Softkey Traffic is now displayed on the map TERRAIN AWARENESS amp WARNING SYSTEM HTAWS DISPLAY A WARNING Do not use HTAWS information for primary terrain avoidance HTAWS is intended only to enhance situational awareness NOTE The data contained in the HTAWS databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 03 AEN 640 S24V oipny uddx svo siu umnnsul Tuo2 AEN iui Duruue d nubi s mp oold paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 70 NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area Displaying the HTAWS Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select HTAWS Page Changing the HTAWS Page view 1 Press the VIEW Softkey 2 Press the 360 or ARC Softkey to select the desired view Or 1 Press the MENU Key 2 Select View Arc or View 360 and press the ENT Key to chan
35. short range weather avoidance 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Wamingstentane amp Notet GARMIN ee WARNING Do not use datalink weather products e g XM WX Satellite Weather GFDS World Wide Weather or FIS B for hazardous weather penetration Weather information provided by these products is aged by up to several minutes and may not depict actual weather conditions as they currently appear WARNING Use of the Stormscope is not intended for hazardous weather penetration thunderstorm penetration Stormscope information as displayed on the G1000H MFD is to be used only for weather avoidance not penetration WARNING The Garmin G1000H as installed in the Bell 407GX rotorcraft 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 G1000H lt is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons G1000H operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsibl
36. special or consequential damages that result from the use or inability to use the software or related documentation even if AOPA or an AOPA authorized representative has been advised of the possibility of such damages User agrees not to sue AOPA and to the maximum extent allowed by law to release and hold harmless AOPA from any causes of action claims or losses related to any actual or alleged inaccuracies in the information Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to you September 2011 190 01254 00 Rev B Printed in the U S A A GARMIN Warnings Cautions E Notes e e 6 6G WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The terrain avoidance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoid
37. temperature is too low to operate correctly Allow units to warm up to GIA2 COOLING GIA2 temperature operating temperature 00 low GIA1 COOLING GIA1 over temperature The GIA1 and or GIA2 temperature is too high If GIA2 COOLING GIA2 over problem persists the system should be serviced temperature GIA1 SERVICE GIA1 needs GIA2 SERVICE GIA2 needs service Return the unit for repair service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The system should be serviced 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX So1nje24 aoueplony s mp oold 4 AEN 540 yi oipny uddx Svol sjueumasu paezey nubi Mbi jeuonippy uoneiedo Jeuuouqy EY x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix nd Annunciations amp Alerts A GARMIN GIA 63H MESSAGE ADVISORIES CONT Message HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted Comments A GIA mismatch has been detected where only one is SBAS capable MANIFEST GIA1 software ismatch communication halted ANIFEST GIA2 software ismatch communication halted The GIA1 and or GIA 2 has incorrect softwar
38. the Navigation 53 XM WX Satellite Weather Optional Worldwide Weather ssssseeeeenennnnnnnnnn Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN LLL Table of Contents Traffic Systems eed ederet ea ien died bands 67 Terrain Awareness amp Warning System HTAWS Display 69 ADDITIONAL FEATURES nnne Synthetic VISION Terminal Procedure Charts AOPA Airport Directory sssssssseeeenenenenn nennen Satellite Telephone and Data Link Services 77 System Data Logging Optional sss 91 SiriusXM Radio Entertainment 92 Auxiliary Video Optional wwwwwwwwwwm ia 94 ABNORMAL OPERATION Reversionary Mode sssssssssseeeeeenne nennen Abnormal COM Operation Hazard Displays with Loss of GPS Position Unusual Attitudes Dead Reckoning sssssseeenn nennen ANNUNCIATIONS amp ALERTS 01 Warning Messages 01 Caution Messages iin 01 Advisory Messages desinet anta ae eh e RHET REESE RETE 03 Safe Operating Annunciation 03 HTAWS
39. turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Press the 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 for a stored flight plan a Press the FPL Key on the MFD b Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor d Turn the large FMS Knob to highlight the desired flight plan e Press the EDIT Softkey Turn the large FMS Knob to highlight the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key Once all changes have been made press the FMS Knob to remove the cursor INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 2 3 46 Press the FPL Key on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254
40. when either Q or MGT fall below takeoff limits Dual Tachometer The dual tachometer displays rotor speed NR and power turbine speed NP as a percentage of maximum rotation A readout for NR is provided The long pointer represents NR along the gauge scale NP is shown with the short pointer A white tick mark represents the FADEC normal governing point When Quiet Mode is active a magenta reference bug is shown on the tachometer to indicate the Quiet Mode governing point POWER ASSURANCE CHECK NOTE Follow the procedures in the Rotorcraft Flight Manual RFM for configuring the helicopter for the power assurance check prior to activating the feature on the G1000H 1 If the Particle Separator or Snow Baffle are installed proceed to step 2 If neither are installed proceed to step 7 2 Tum the large FMS Knob to select the AUX Page group 3 Turn the small FMS Knob to select System Setup If necessary press the SETUP 1 Softkey to display the System Setup 1 Page 4 Press the FMS Knob momentarily to activate the flashing cursor 5 Turn the large FMS Knob to highlight the desired option field in the Inlet Box 6 Turn the small FMS Knob one dick to the right to select ON or one click to the left to select OFF 7 Press the ENGINE Softkey to display the Engine Page 8 Press the PWR CHK Softkey When the power assurance check is activated a PWR CHECK box is displayed containing a progress meter If the helicopter c
41. 00 Rev B GARMIN ight Planning 4 5 6 Turn the large FMS Knob to highlight the desired flight plan Press the INVERT Softkey Invert and activate stored flight plan is displayed With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location COPY A FLIGHT PLAN 1 2 3 4 5 6 Press the FPL Key on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be copied Press the COPY Softkey A Copy to flight plan 5 confirmation window is displayed 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 2 3 4 5 6 Press the FPL Key on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be deleted Press the DELETE Softkey A Delete flight plan 22 confirmation window is displayed With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key GRAPHICAL FLIGHT PLAN CREATION 1 2 Press the FPL Key on the MFD
42. 1 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 12 The flashing cursor moves to the barometric setting PRESSURE field Enter the desired baro setting Press the ENT Key when finished Note that in AUTOMATIC page mode the baro setting is provided by the setting entered on the PFD 13 The flashing cursor moves to the air temperature TOTAL AIRTEMP 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 CREATE A USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Turn the large FMS Knob on the MFD to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position 4 Enter the desire d waypoint name 5 Press the ENT Key 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 37 s tin sul sub 5721 oipny uddx UI0JNeN 52 2 Buluuejd AEN Sd5 nubi 2 spay uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instrumen
43. 1 and 12 see a service center as soon as possible to inspect correct wiring This wiring fault can cause fail safe audio not to function See a service center as soon as possible to inspect correct wiring This wiring fault can cause fail safe audio not to function Verify correct orientation from the left right indication on each side of the headset or the position of the boom mic usually attached on left side If the headset is backwards left right position information will be Swapped See a service center as soon as possible to inspect correct wiring This wiring fault can cause fail safe audio not to function Garmin G1000H Cockpit Reference Guide for the Bell 407GX 1 Mono headset in use 1 Use a stereo headset sjueumasu 5721 z 2 gt 3 o uoneiado saunyea4 aoueplony saunpa20Jd Fuluueld AEN Sd5 241V unuuy jeuuouqy jeuonippy paezey xipuaddy x pul iui JUI05JAEN Wfil4 Abnormal Additional Hazard Annun Flight Instruments Flight Planning Nav Com AFCS XPDR Audio EICAS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN 3D Audio Troubleshooting Symptom s Solution s 30 audio left 1 Aircraft wired for mono 1 See a service center to wire the message heard intercom installation for stereo headsets in left ear only no audio heard in right ear 3D audio right Incorre
44. 213 sjueumasu piezeH ubi wio gt AeN 4461 jeuonippy uoneiedo Jeuuouqy WA EST x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix n Annunciations 8 Alerts A GARMIN FLIGHT PLAN IMPORT EXPORT MESSAGES CONT Flight Plan Import Export Results User waypoint database full Not all loaded Description 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 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMI N Appendix APPENDIX
45. 5 Ifyou have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000H system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the G1000H Pilot s Guide for this aircraft Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Paai Renisions Change Summary 190 01254 00 RevA Initial release E Date of Revision Affected Pages September 2011 Update SiriusXM product references Updated Iridium registration procedure Added other GDU 12 01 parameters Added Worldwide Weather Added 3D audio Added Voice Recognition Added MV DB update procedure 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX RR 1 Record of Revisions GARMIN Blank Page RR 2 Garmin G1000H Cockpit Reference Guide for the Bell 4076X
46. 9 Altitude volume 69 AOPA s Airport Directory 76 Barometric Altitude Minimums 3 4 Barometric pressure 127 C CDI 1 119 Channel Presets 94 ChartView 74 75 CLD TOP Softkey 64 Clearance player 14 Clearance Recorder 14 Code selection softkeys 11 COM 11 13 97 Crevv Alerting System CAS Messages 10 15 190 01254 00 Rev B Index D Data reports 91 DB Mismatch 131 134 DCLTR Softkey 74 Dead Reckoning 99 Declutter 98 124 130 Direct to 31 DME 11 DR mode 99 100 E Edit a flight plan 46 F Flight path marker 73 Flight plan import export messages 121 122 FliteCharts 74 75 Frequency Transfer 13 Fuel Flow FFLOW GPH 6 H Heading Preset Mode 2 120 126 127 Horizon heading 73 HSI double green arrow 12 HSI magenta arrow 12 HSI single green arrow 12 Inset Map 123 124 130 IOI 104 lridium satellite network 77 78 81 Garmin G1000H Cockpit Reference Guide for the Bell 407GX Index 1 sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 S24JV oipny uddx sY213 sjuaumasu jeuonippy 2 nubi Tuo2 NeN wb uoneiedo Jeuuouqy Sue v unuuy 1221 ow Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS KPDR Audio EICAS Instruments Abnormal Operation Annun Alerts T Appendix Index J Jeppesen 75 L Low speed data 78 M Magnetic Field Variation Database Update 134 Map panning 54 Message advisories 107 120 METAR 53
47. AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Flight Instruments GARMIN 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 ENABLE HEADING PRESET MODE 1 Press the SET HDG Softkey on the PFD The system is in Heading Preset Mode HPM as indicated by displaying SET to the left of the heading value 2 Press the HDG and or HDG Softkeys to slew the heading value to the desired setting Or Set the Selected Heading Bug to the desired heading value then press the HDG SYNC Softkey DISABLE HEADING PRESET MODE Press the HPM OFF Softkey on the PFD to manually disable Heading Preset Mode Or Heading Preset Mode automatically disables after eight minutes If there is more than 10 difference between the Heading Preset value and the magnetic heading when Heading Preset Mode is disabled the heading value is displayed in yellow and ALN will be displayed to the left of the heading When the magnetic heading has properly aligned the heading value will be displayed in white and ALN will no longer be displayed Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN Flight instruments GENERIC T
48. APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Note that NOTAMS are only available with ChartView 3 Press the GO BACK Softkey to return to the previous page 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 75 xipuaddy suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 S24JV olpny uqax 5921 sjuauimasu junuuy Jeuuouqy Jeuonippy p EzeH ubi wo gt AeN ubi x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Addend Features GARMIN View Charts from the Active Flight Plan Page 1 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to select the departure airport destination airport departure arrival or approach 3 Press the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected 4 Press the GO BACK Softkey to return to the previous page Change Day Night View 1 While viewing a chart press the MENU Key to display the Page Menu OPTIONS 2 Tum the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options 4 Turn the small FMS Knob to choose betwe
49. AeN Sd5 S24V oipny uadx svola siu u nnsul Tu102 AEN 346 eouepioAy paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 90 A GARMIN To save and connect the selected network a Press the ENT Key A checkmark is placed in the checkbox and the cursor moves to the airport field b Using the FMS Knobs enter an airport identifier to be associated with the saved network This aids in identifying the network later in the event of duplicate network names Press the ENT Key The cursor moves to CONNECT d Press the ENT Key again to connect to the selected network Editing a Saved Network 1 2 3 4 5 6 1 8 9 While viewing list of saved networks press the FMS Knob to activate the cursor Turn either FMS Knob to highlight the network to be edited Pressing the ENT Key at this point will check or uncheck the AUTO CONNECT checkbox When a checkmark is present the system will automatically connect to the network when within range Press the EDIT Softkey The cursor now appears in the CONNECTION SETTINGS window Turn the large FMS Knob to select the network attribute to be edited Turn the small FMS Knob to begin editing the field
50. BSTACLE CAUTION OBSTACLE Caution Obstacle Impact Caution 101 Obstacle Voice Callout VCO None None Five Hundred Four Fifty Four Hundred Three Fifty Three Hundred Two Fifty Two Hundred One Fifty One Hundred Fifty HTAWS Alerts Summary Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN HTAWS SYSTEM STATUS ANNUNCIATIONS Annunciations 8 Alerts PFD HTAVV HTAVVS Page Center Aural Alert Type Page Status A D Banner Annunciation Message Annunciation system Test in HTAWS TEST None Progress System Test Pass None HTAWS Test OK HTAMS FAIL HTAWS Failure Failure HTAWS Not HTAWS Not Available LHTAWS N A Available HTAWS FLTA Alerting Inhibited HIANS INH dii HTAWS Availability None HTAVVS Restored Available Reduced Protection RP MODE Mode Enabled MUR MFD Terrain or None one Obstacle database unavailable or invalid HTAWS operating with PFD Terrain or Obstacle databases Terrain or 5 FAIL HTAWS Failure Obstacle database unavailable or invalid on all displays invalid software configuration HTAWS audio fault No GPS position HTAMS NZA HTAWS Not Available HTAWS Available when GPS position returns and HTAWS is not inhibited 190 01254 00 Rev B
51. D 2 Press the FPL Key on the MFD to display the Active Flight Plan Page 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 Press 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 2 Buluuejd AEN Sd5 nubi svo sjuounasu U105 AEN 3461 olpny uqax 52 desired select CANCEL using the FMS press the Key select another existing or empty flight plan and again press the IMPORT Softkey 7 Turn the small FMS Knob to highlight the desired flight plan for importing 8 Press the ENT Key INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 If required press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint 4 Turn the small FMS Knob The Waypoint Information Window is now displayed 5 Enter the new fl
52. G1 000H Integrated Flight Deck Cockpit Reference Guide for the Bell 407GK A GARMIN Copyright O 2011 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software 1237 03 or later for the Bell 407GX Some differences in operation may be observed when comparing the information in this manual to ea Garmi Tel 9 Garmi Tel 5 Garmi ier or later software versions n International Inc 1200 East 151st Street Olathe Kansas 66062 U S A 13 397 8200 Fax 913 397 8282 n AT Inc 2345 Turner Road SE Salem OR 97302 U S A 03 391 3411 Fax 503 364 2138 n Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton S040 9RB U K Tel 4 Garm Tel 8 STI and i Web 410870 8501241 Fax 44 0870 8501251 n Corporation No 68 Jangshu 2nd Road Shiir Taipei County Taiwan 86 02 2642 9199 Fax 886 02 2642 9099 or after hours emergency aircraft on ground AOG technical support for Garmin panel mount ntegrated avionics systems please contact Garmin s AOG Hotline at 913 397 0836 Site Address www garmin com Except as expressly provided herein no part of this manual may be reproduced copied trans mitted disseminated downloaded or stored in any storage medium for any purpose Without the express written permission of Garmin Garmin hereby grants permission to download a single co
53. IMER 1 2 3 Press the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted Turn the small FMS Knob to display the UP DOWN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it starts counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window CONFIGURE VSPEED BUGS INDIVIDUALLY 1 2 3 4 5 6 Press the TMR REF Softkey Turn the large FMS Knob to highlight the desired Vspeed Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to the speed Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field Turn the small FMS Knob clockwise to ON or counterclockwise to OFF To remove the window press the CLR Key or the TMR REF Softkey SET BAROMETRIC MINIMUM DESCENT ALTITUDE 1 2 3 4 5 6 7 Press the TMR REF Softkey Turn the large FMS Knob to highlight the OFF BARO field to the right of MINIMUMS Turn the small FMS Knob clockwise to BARO Press the ENT Key Use the small FMS Knob to enter the desired altitude Press the ENT Key To remove the window press the CL
54. JV olpny uqax Sv l4 sjueuimasu junuuy Jeuuouqy Jeuonippy p EzeH BITTE u05 AeN ubiu x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN Incoming Calls When viewing MFD pages other than the AUX TELEPHONE Page a pop up alert will be displayed The pop up alert may be inhibited at times such as during takeoff In addition to the pop up alert a ringing phone symbol will be displayed to the right of the MFD page title Also the voice alert Incoming Call will be heard on the selected cockpit audio Answering an incoming call 1 Press the TEL Key on the appropriate audio panel 2 Select the ANSWER Softkey on the MFD Or While viewing the AUX TELEPHONE Page NOTE The Push to Talk switch is not utilized for telephone communication The microphone is active after selecting the ANSWER Softkey and stays active until the call is terminated 1 Press the TEL Key on the appropriate audio panel 2 Press the MENU Key to display the Page Menu 3 Turn either FMS Knob to place the cursor on Answer Incoming Call 4 Press the ENT Key Selecting the IGNORE Softkey will extinguish the pop up window and leave the current call unanswered Selecting the IGNRE ALL Softkey will extinguish the pop up window for the current and
55. Knob or the ENT Key to scroll through the PIREP text 7 Press the FMS Knob or the CLR Key to close the PIREP text window and return to the GFDS Weather Data Link Page To display the PIREP or AIREP legend select the LEGEND Softkey when PIREPs or AIREPs are selected for display The PIREP color is determined by the type routine or urgent Winds Aloft Winds Aloft data shows the forecasted wind speed and direction at the surface and at selected altitudes Altitude can be displayed in 3 000 foot increments up to 42 000 feet MSL DispLayinc Winns ALOFT DATA 1 Select the GFDS Weather Data Link Page 2 Select the MORE WX Softkey 66 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN 3 Select the WIND Softkey 4 Select the desired altitude level SFC surface up to 42 000 feet Select the NEXT or PREV Softkey to cycle through the altitude softkeys The WIND Softkey label changes to reflect the altitude selected To display the Winds Aloft legend select the LEGEND Softkey when Winds Aloft is selected for display TRAFFIC SYSTEMS Hazard Avoidance f Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE softkeys are displayed Ifa Traffic Advisory System TAS is configured STANDBY NORMAL TEST and ALT MODE softkeys are displayed Traffic Symbol Description Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical sepa
56. Knob to select REPORTS DATA LINK 3 If necessary press the WI FI Softkey to display the AUX VVI H SETUP Page Setting Up a New Wi Fi Connection 1 Press the AVAIL Softkey on the MFD A list of available networks will be displayed in the AVAILABLE NETWORKS window Signal strength is shown for each network as well as security methods and whether the network has been saved in the system s memory 2 If necessary press the RESCAN Softkey to have the system scan again for available networks 3 Press the FMS Knob to place the cursor in the list of networks 4 Turn either FMS Knob to select the desired network 5 Press the CONNECT Softkey 6 If the network is secured enter the necessary passcode Use the FMS Knobs to enter the desired alpha numeric characters Press the CAP LOCK Softkey to enter upper case letters If there is no security associated with the network proceed to step 9 7 Press the ENT Key OK will be highlighted 8 Press the ENT Key again 9 The SAVE SETTINGS window is now displayed with the cursor highlighting SAVE CONNECTION 10 easier at a later time To connect the selected netvvork vvithout saving a Turn the large FMS Knob to move the cursor to highlight CONNECT b Press the ENT Key 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX The selected network can be saved to system memory to make reconnection 89 s mp o4d Buruuejd
57. Manually testing the HTAVVS System 1 Select the HTAWS Page 2 Press the MENU Key 3 Select Test HTAWS System and press the ENT Key to confirm the selection 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX AEN 540 S24V oipny uddx svo siu umnnsul Tuo2 AEN iui Duruue d u u aoueploay s mp oold paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Muting Unmuting Caution Alerts 1 2 1 2 Turn the large FMS Knob to select the HTAWS Page on the MFD Press the MUTE CTN Softkey Or Press the MENU Key Select Mute Active Caution or Unmute Active Caution choice dependent on current state and press the ENT Key Inhibiting enabling PDA and FLTA alerting 1 2 1 2 Select the HTAWS Page Press the INHIBIT Softkey to inhibit or enable HTAWS choice dependent on current state Or Press the MENU Key Select Inhibit HTAVVS or Enable HTAVVS choice dependent on current state and press the ENT Key Configuring VCO alerting altitudes 1 2 3 4 5 6 72 Turn the large FMS knob to select the AUX System Setup Page If the Aux System Setup 2 Page is not alr
58. ORIES A GARMIN Message GSR1 FAIL GSR1 has failed Comments A failure has been detected in the 1 GSR 56H The system should be serviced GDL 59H MESSAGE ADVISORIES Message GDL59 CONFIG GDL 59 config error Config service req d Comments GDL 59H configuration settings do not match those of backup configuration memory The system should be serviced GDL59 FAIL GDL 59 has failed A failure has been detected in the GDL 59H The receiver is unavailable The system should be serviced 02 GDL59 SERVICE GDL 59 needs service Return unit for repair A failure has been detected in the GDL 59H The system should be serviced ab GDL59 RTR FAIL The GDL 59 router has failed REGISTER GFDS Data services are inoperative register w GFDS A failure has been detected in the GDL 59H router The system should be serviced The GDL 59H is not registered with Garmin Flight Data Services or it s current registration data has failed authentication MANIFEST GDL software mismatch communication halted The GDL 59H has incorrect software installed The system should be serviced GDL 69AH MESSAGE ADVISORIES Message Comments GDL69 CONFIG GDL 69 config error Config service req d GDL69 FAIL GDL 69 has failed GDL 69AH configuration settings do not match those of backup configuration memory The G1000H system should
59. Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Press the ENT Key Repeat step 10 to enter the next waypoint name Press the ENT Key The cursor is displayed in the RAD radial field for the second waypoint Enter the desired radial from the reference waypoint Press the ENT Key Press the FMS Knob to remove the flashing cursor 39 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX sjuauimasu UATE 5721 oipny uddx UI0JNeN 52 2 Buluuejd AEN Sd5 nubi eouepioAy 2 Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM 40 1 2 3 4 5 6 1 8 9 10 ANOTHER WAYPOINT Turn the large FMS Knob on the MFD to select the WPT page group Turn the small FMS Knob to select the User WPT Informa
60. R Key or the TMR REF Softkey 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX zn g 2 o 2 a sualy uonesado saunjeaj 2 Bbuluuejd AEN 5649 24V oipny uadx svoli junuuy jeuuouqy Jeuonippy paezey nubi xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EICAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Flight Instruments GARMIN SET BAROMETRIC RADAR ALTIMETER RA OPTIONAL MINIMUM DESCENT ALTITUDE 1 Press the TMR REF Softkey 2 Tum the large FMS Knob to highlight the OFF BARO RAD ALT field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to select BARO or RAD ALT 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 To remove the window press the CLR Key or the TMR REF Softkey DISPLAYING WIND DATA 1 Press the PFD Softkey 2 Press the WIND Softkey to display wind data to the left of the HSI 3 Press one of the OPTN softkeys to change how wind data is displayed 4 Toremove the Wind Data Window press the OFF Softkey CHANGING HSI FORMAT 1 Press the PFD Softkey 2 Press the HSI FRMT Softkey 3 Press the 360 HSI Softkey to display the full size HSI Or Press the ARC HSI Softkey to display the arc style HSI 4 Garmin G1000H Cockpit Reference Guide for th
61. RMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG 1 Press the PFD Softkey 2 Press the STD BARO Softkey to set standard barometric pressure CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Press the PFD Softkey to display the second level softkeys 2 Press the ALT UNIT Softkey 3 Press the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Press the HPA Softkey to display the barometric pressure setting in hectopascals 4 Press the BACK Softkey to return to the top level softkeys CHANGE NAVIGATION SOURCES 1 Press the CDI Softkey to change from GPS to VOR1 or LOC1 This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD 2 Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the light blue tuning box over the NAV2 standby frequency 3 Press the CDI Softkey a third time to return to GPS 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX sualy uonesado saunjeaj uepjoay sampadoj Buruuejd AEN 5649 24V oipny uadx svoli junuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun g l E E E 5 4 EICAS
62. Traffic Information Service TIS coverage area Traffic Traffic Played when a Traffic Advisory TA is issued Skywatch TAS system TAS System Test Played when the GTS 800 TAS system passes a pilot initiated self Passed test TAS System Test Played when the GTS 800 TAS system fails a pilot initiated self test Failed One o clock through Intruder bearing GTS 800 only 106 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Annunciations 8 Alerts Voice Alert Description High Low Same Altitude if within 200 feet of own altitude or Altitude not available Intruder relative altitude GTS 800 only than ten miles Less than one mile One Mile through Ten Miles or More Intruder distance GTS 800 only 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 PFD1 SERVICE PFD1 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair The MFD and PFD are not communicating with each other The system should be serviced The PFD and or MFD self test has det
63. a504d Buruue d AEN Sd5 52 olpny gqax Sv213 s3u u n sul piezeH ubi U105 AEN ubiu saunjeaj jeuonippy xipuaddy suelv junuuy x pul Flight Instruments Nav Com KPDR Audio Flight Planning Hazard Additional Annun EICAS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index Abnormal Operation UNUSUAL ATTITUDES A GARMIN The PFD declutters when the aircraft enters an unusual attitude Only the primary functions are displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the aircraft experiences unusual attitudes 98 Traffic Annunciations AFCS Annunciations Flight director Command Bars Inset Map Temperatures DME Information Window Wind Data Selected Heading Box Selected Course Box Transponder Status Box System Time PFD Setup Menu Windows displayed in the lower right corner of the PFD Timer References Nearest Airports Flight Plan Messages Procedures DME Tuning Barometric Minimum Descent Altitude Box Glideslope Glidepath and Vertical Deviation Indicators Altimeter Barometric Setting Selected Altitude VNV Target Altitude Garmin G1000H Cockpit Reference Guide for the Bell 407GX Extreme Pitch Indication 190 01254 00 Rev B GARMIN Abnormal operation DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000H detects an in
64. al flight plan waypoint When all waypoints have been entered press the FMS Knob to remove the cursor Creating a stored flight plan 1 2 3 4 5 6 7 Press the FPL Key Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page Press the NEW Softkey or press the MENU Key highlight Create New Flight Plan and press the ENT Key to display a blank flight plan for the first empty storage location Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway vvaypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key Repeat step numbers 4 and 5 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Garmin G1000H Cockpit Reference Guide for the Bell 4076X 190 01254 00 Rev B A GARMIN Flight Planning IMPORT A FLIGHT PLAN FROM AN SD CARD NOTE See the Annunciations amp Alerts section for flight plan import message descriptions 1 Insert the SD card containing the flight plan in the top card slot on the MF
65. alid There is a problem with the GFDS registration Contact Garmin Flight Data Services at 1 866 739 5687 in the United States or 913 397 8200 ext 1135 for assistance GFDS Server Temporarily Inop The GFDS weather data server is temporarily out of service but s expected to return to service in less than 30 minutes GFDS Server Inop The GFDS weather data server will be out of service for at least 30 minutes Invalid Coverage Area The weather data request coverage area does not contain at least one of the following a waypoint a flight plan or a flight plan destination Verify at least one of the coverage options is enabled checked and contains required criteria then re send the data request 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX AEN Sd5 S24V oipny d4adx sv siu umn sul u102 AEN Duruue d nubi e uepioAy s mp oold paezey Suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Weather Request Description Status Message No GFDS Subscription 1 The system is not be currently subscribed to GFDS or the access Reduce Request Area code is incorrect Verify the access code Con
66. all future incoming calls and leave the current call unanswered Selecting the TEL Softkey will display the AUX TELEPHONE Page al lowing additional call information to be viewed before answering Disabling incoming call alerts 1 With the AUX TELEPHONE Page displayed press the MENU Key on the MFD to display the Page Menu 2 Turn either FMS Knob to place the cursor on Disable Incoming Call Alerts 3 Press the ENT Key The voice and pop up alert will not be displayed now when an incoming call is received 80 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Outgoing Calls Voice calls can be made from the cockpit through the Iridium Satellite Network Additional Features To make a call from the cockpit using the Iridium satellite network 1 Press the TEL Key on the audio panel 2 Select the DIAL Softkey on the MFD 3 Enter the desired telephone number country code first by selecting the number softkeys on the MFD 4 Press the ENT Key OK is highlighted 5 Press the ENT Key The system will begin calling the number When the phone is answered the connection is established To exit the call select the HANGUP Softkey Placing The Call on Hold Select the HOLD Softkey on the MFD Or 1 Press the MENU Key to display the Page Menu 2 Turn either FMS Knob to place the cursor on Put Current Call On Hold 3 Press the ENT Key The phone is now isolated
67. ance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000H GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74H 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 G1000H PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000H system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on the G1000H Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING 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
68. and turn the small FMS Knob to select the desired diameter and route width of the request then press the ENT Key Turn the large FMS Knob until the SEND REQ button is highlighted Press the ENT Key to initiate the request immediately or press the FMS Knob to return to the GFDS Data Link Page without requesting data e During a GFDS Data Request the Request Status box initially displays Contacting GFDS Once a connection is established the Request Status Box displays Receiving Wx Data Time Remaining with an estimated data transfer time either minutes or seconds If desired the GFDS Data Request window may be closed while the data request is processing by pressing the FMS Knob the data request will continue to process in the background GFDS Data Requests typically take between 1 to 4 minutes to complete depending on the size of the selected weather coverage area and Iridium signal strength The system retrieves all available Worldwide Weather products within the selected coverage area during an initial GFDS Data Request regardless of which products if any are currently enabled for display On subsequent requests previously retrieved textual data such as METARs and TAFS is retained if it has not expired while new textual weather data matching the current coverage area and all graphical weather data is downloaded during every data request If the system cannot complete a GFDS weather data request one or more mes
69. ard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Map Panning Information Weather Data Link Page 1 2 Push in the Joystick to display the panning arrow Move the Joystick to place the panning arrow on AIRMETs TFRs METARs or SIGMETs 3 Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information XM WX Satellite Weather Products and Symbols Wx Product Status Icons Description US 3m CN Bm R NEXRAD Available for the US and Canada The age of the displayed data for each is shown at the right om ECHO TOP The age of the displayed data is shown at the right Not displayed when CLOUD TOP is displayed b 12m CLOUD TOP The age of the displayed data is shown at the right Not displayed when ECHO TOP is displayed 3m i XM LIGHTNING The age of the displayed data is shown at the right 2m SIGMET 2m AIRMET 5m Fus 8m CN 8m Ame Sa ok CELL MOVEMENT The age of the displ
70. aso Hsi Anc nsi ll Leecx mse LL Tr TL erm T om TT or L 1 L L Lssex L v s F3 V3 V3 F3 F3 F3 n8 EN nn nm m PATHWAY SYN TERR HRZN HDG APTSIGNS BACK MSG E V3 F3 F3 nios EN EN n n n 74 PFD Configuration Softkeys Duruue d nf s snp old aoueplony paezey Level 1 Level 2 Level 3 Description saunqea4 jeuonippy PFD Displays second level softkeys for additional PFD configurations SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features uoneiedo Jeuuouqy PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction Sue v unuuy gt 5 5 o z m x HRZN HDG Displays compass heading along the Zero Pitch line x pul 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Additional Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix A GARMIN Level 1 Level 2 Level 3 Description APTSIGNS Displays position markers for airports DFLTS WIND OPTN 1 OPTN 2 OPTN 3 OFF DME BRGI HSI FRMT 360 HSI ARC HSI BRG2 SET HDG HDG SYNC HDG HDG within approximately 15 nm of the current aircraft position Airport identi
71. assenger Copilot 2 passenger Configuration j 9 if Configures Voice Response Copilot is crew Copilot as Copilot flight crew arker Beacon Markar or audio on i i off refer luminate Extinguish MKR Beacon MKR Mute marker or MUTE Marker mute to Marker MUTE Annunciator arker mute Becan section for details Cursor off or Cancels i cursor when Cursor Cursor cancel or l Cursor is removed cursor is Cancel cursor flashing 190 01254 00 Rev B 25 Garmin G1000H Cockpit Reference Guide for the Bell 407GX siu umnnsu 5721 a 2 gt o SoJnjeaJ saunpa20Jd Fuluueld AEN Sd5 2 2 jeuonippv uoneiedo Jeuuouqy Sue v unuuy xipuaddy x pul fid JUI05 AEN Wfil4 Hight EICAS Instruments Nav Com 25 x a r gt Annun Abnormal Additional Hazard Flight Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS Index Nav Com XPDR Audio Panel A GARMIN Man squelch volume down Control Spoken Command Action Confirmation of Action Manual squelch or Toggles Illuminate Extinguish MAN Man squelch manua SQ Annunciator q squelch Manual squelch threshold up or Increases Manual squelch volume up or manual Manual squelch threshold Man squelch threshold up or 20 77 p threshold Ma
72. ay PRECIPITATION LIMITATIONS Radar images may have certain limitations Radar base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics wet hail vs rain For example it is not possible to distinguish between wet snow wet hail and rain e Radar base reflectivity is sampled at the minimum antenna elevation angle An individual radar site cannot depict high altitude storms at close ranges It has no information about storms directly over the site When zoomed in to a range of 30 nm each square block on the display represents an area of four square kilometers 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 63 oipny uddx SP EI siu uinnsu UI05 AEN ubiu 52 AEN 540 buluueld Wil aoueploay s mp oold paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN The following may cause abnormalities in displayed radar images Ground clutter Strobes and spurious radar data Sun strobes when the radar antenna points directly at the sun nterference from buildings or mountains which may cause shadows Metallic dust from military aircraft which can cause alterations
73. ayed data is shown at the right SIGMET amp AIRMET The age of the displayed data for each is shown at the right METAR Available for the US and Canada The age of the displayed data for each is shown at the right SURFACE ANALYSIS with CITY FORECAST The upper symbol depicts Surface Analysis The lower symbol depicts City Forecast The age of the displayed data for each is shown at the right The selected forecast period is Shown at the bottom 54 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Hazard Avoidance Wx Product Status Icons Description 4m FREEZING LEVEL The age of the displayed data is shown at the right us 8m CN 12m 3000FT WINDS ALOFT Available for the US and Canada The age of the displayed data for each is shown at the right The altitude selection is shown at the bottom COUNTY WARNING The age of the displayed data is shown at the right 2m CYCLONE WARNING The age of the displayed data is shown at the right AIREP The age of the displayed data is shown at the right 1 68m 21000F1 PIREP The age of the displayed data is shown at the right Urgent Pireps are displayed in yellow TURBULENCE The age of the displayed data is shown at the right The altitude selection is shown at the bottom 4m 6000FT ICING POTENTIAL The age of the displayed data is shown at the right
74. aypoints Create a User Waypoint Defined by a Radial amp Distance from Another Waypoint 40 Delete a User WAayPONN w nnn 41 Create a Flight Plan 42 Import a Flight Plan from an SD Card 43 Insert a Waypoint in the Active Flight 77 555 7 43 Enter an Airway in a Flight Plan 44 Invert An Active Flight Plan 45 Remove a Departure Arrival Approach or Airway from a Flight Plan 45 Store a Flight Plan tie ere cem nitet dicat Edit a Stored Flight Plan Delete a Waypoint from the Flight Plan ss Invert and Activate a Stored Flight Plan Copy a Flight Plan Delete a Flight Plan Graphical Flight Plan Creation Export a Flight Plan to an SD Card PROCEDURES a a a asa Load and Activate a Departure Procedure Activate A Departure Leg ssssesseeennennnnnnnnnes Load An Arrival Procedure Activate An Arrival Leg sse Load and or Activate an Approach Procedure 50 Activate An Approach in the Active Flight 7 51 Activate a Vector to Final Approach Fix sssssse 52 Activate A Missed Approach in the Active Flight Plan 52 HAZARD AVOIDANCE ici sss scien nla tee E Ri 53 Customizing the Hazard Displays on
75. configured by a Garmin authorized service facility in order to use some database features If an error occurs during synchronization an error message will be displayed followed by the affected display in the Sync Status section of the Database Window 1f synchronization completes on one display but an error occurs on another the error message will be displayed with the affected diaplays listed after it When an error message is displayed the problem must be corrected before synchronization can be completed A power cycle is required to restart synchronization when Card Full or rr is shown Error Message Description Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted Timeout System timed out prior to the database transfer completing 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax Svo sjuauimasu jeuonippy 2 Wil Tuo2 NeN nubi uoneiedo Jeuuouqy Sue v unuuy m bid Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN L
76. ct aircraft wiring See a service center as soon as message heard right channel used for possible to inspect correct wiring in right ear only mono instead of left or This wiring fault can cause fail safe no audio heard left right swapped audio not to function in left ear 3D Audio Troubleshooting VOICE RECOGNITION Voice Recognition allows the pilot and optionally copilot to control the GMA 350H using spoken commands To activate Voice Recognition push and hold the Push To Command PTC button while speaking a command When the Push To Command button is released the GMA 350H will respond If a command is correctly interpreted by the GMA 350H a positive acknowlege ment chime will be played and the pilot should verify that the correct button selection is indicated by the triangular annunciator lights Alternatively some commands will be indicated by a voice response from the GMA 350H If the desired modes are not indicated by annunciator lights or a voice response the pilot should repeat the com mand by using the Push To Command button or by manually using the front panel controls of the GMA 350H If a command is incorrectly interpreted by the GMA 350H a negative acknowlege ment tone will be played The pilot should repeat the command by using the Push To Command button or by manually using the front panel controls of the GMA 350H In the event of any abnormal Voice Recognition operation at any time the front panel contro
77. d by SiriusXM Radio Service is approved only for weather avoidance not penetration Displaying XM WX on the Navigation Map Page 1 Press the MAP Softkey 2 Press the NEXRAD or XM LTNG Softkey to display the desired weather Press the applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 Tum the large FMS Knob to select the WPT Page Group 2 Turn the small FMS Knob to select the Airport Information Page 3 Press the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Displaying Weather on the Weather Data Link Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Data Link Page 3 Press the available softkeys to select the desired XM weather product 4 Press the LEGEND Softkey to view the legends for the selected products If necessary turn either FMS Knob to scroll through the list Press the small FMS Knob or the ENT Key to return to the map 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 3 AEN Sd5 S24V oipny uadx 59213 siu umn sul u102 AEN fila Duruue d ni e uepioAy s mp oold paezey SH V uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Haz
78. d effort can be saved in typing text messages that are used repeatedly by saving these messages as a predefined message Create a Predefined Text Message 1 2 3 4 5 6 1 8 9 10 11 12 While viewing the AUX TEXT MESSAGING Page press the MENU Key to display the Page Menu Turn either FMS Knob to select Edit Predefined Messages Press the ENT Key The PREDEFINED MESSSAGES view is now displayed Press the NEW Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Draft New Predefined Message c Press the ENT Key The PREDEFINED SMS TEXT MESSAGE Window is now displayed The cursor is displayed in the TITLE field Enter the desired message title Entry can be accomplished through the FMS Knob and softkeys on the MFD The FMS Knob is used to enter letters and numbers or numbers can be entered from the MFD by pressing the NUMBERS Softkey Press the CAP LOCK Softkey to create upper and lower case alpha characters Special characters can be accessed by pressing the SYMBOLS Softkey Press the ENT Key The cursor is now displayed in the MESSAGE field Enter the desired message using any combination of entry methods as described in step 5 Press the ENT Key Press the SAVE Softkey The new predefined message is now shown in the displayed list Pressing the CANCEL Softkey will delete the message without saving Press the MENU Key to di
79. database Ensure that the terrain card is PFD1 DB ERR PFD1 terrain database e 0 exists properly inserted in display Replace terrain card If problem persists the system should be serviced Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Annunciations 8 Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing Comments The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists The MFD and or PFD detected a fai lure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists the system should be servi ced MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstade database missing The obstacle database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists The MFD and or PFD detected a fai lure in the Safe Taxi database Ensure that the data card is properly inserted Replace data ca persists the system should be servi d If problem ced MFD1 DB ERR MFD1 C
80. display now starts in normal mode Do not remove power while the display is starting Press the ENT Key to acknowledge the startup screen Turn the large FMS Knob to select the AUK Page group on the MFD Turn the small FMS Knob to select the System Status Page The new database is copied to the SD card in the bottom card slot of each PFD Progress can be monitored in the SYNC STATUS field When copying is finished Complete is displayed NOTE During the synchronization process version differences between standby navigation databases will exist This will result in the system displaying a DB Mismatch alert for the standby navigation databases This alert will remain until the next power cycle Turn system power OFF Remove the SD card from the top card slot of the MFD Turn system power ON Press the ENT Key to acknowledge the startup screen Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show standby navigation database information for each display MFD1 DB PFD1 DB Verify the correct standby navigation database cycle information is shown for each display Magnetic Field Variation Database Update At startup the system compares this version of the MV DB with that presently being used by the AHRS GRS If the system determines the MV DB needs to be updated a prompt is displayed on the Navigation Ma
81. dx 5219 sjuauimasu J05 AeN sub Duruue d yi aoueploay s mp oold paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 3 Use the FMS Knob to enter the desired airport and press the ENT Key 4 Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text Note that the METAR text must be completely scrolled through before scrolling through the TAF text To display the METAR legend on the GFDS Weather Data Link Page select the LEGEND Softkey when METARs are selected for display PIREPs Pilot Weather Reports PIREPs describe in flight weather encountered by pilots A PIREP may contain adverse weather conditions not forecasted such as low in flight visibility icing conditions wind shear turbulence and type of aircraft flown PIREPs are issued as either Routine UA or Urgent UUA DisPLAYiNG PIREP 1 Select the GFDS Weather Data Link Page 2 Select the MORE WX Softkey 3 Select the PIREPS Softkey 4 Press the RANGE Knob and pan to the desired weather report A gray circle will appear around the weather report when it is selected 5 Press the ENT Key The PIREP text is first displayed in a decoded fashion then as raw text 6 Use the FMS
82. e installed The system should be serviced ANIFEST GFC software ismatch communication Incorrect servo software is installed or gain settings are incorrect ANIFEST COM1 softw ANIFEST COM2 softw ismatch communication halted 1 and or COM2 software mismatch The G1000 system should be serviced ANIFEST NAV1 software ismatch communication halted ANIFEST NAV2 software ismatch communication halted m M m M m M mismatch communication M m M m M m NAV1 and or NAV2 software mismatch The G1000 system should be serviced COM1 CONFIG COM config rror Config service req d CD COM2 CONFIG COM2 config error Config service req d COM and or COM2 configuration settings do not match backup configuration memory The G1000 system should be serviced COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the system should be serviced COM1 SERVICE COM1 needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may still be usable The system should be serviced when possible
83. e Bell 407GX 190 01254 00 Rev B A GARMIN Engine Indication S Gew Alerting System ENGINE INDICATION SYSTEM uB TOTAL ai sui TOTAL PRESS MFD EIS Display Normal EIS Display Reversionary 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Sjueuinijsu BUT SE xipueddy Suelv uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld AEN Sd5 241V olpny uqax unuuy jeuuouqy jeuonippy paezey wd U105 AEN x pul Flight Instruments EICAS C X 035 Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS Procedures GPS Nav Alerts Operation Features Appendix Index 4 Engine Indication amp Crew Alerting ayla GARMIN Engine Oil Pressure Displays pressure of oil supplied to the engine P Oil Temperature Indicator T Transmission Oil Pressure P Transmission Oil Temperature T Ammeter A Voltmeter V Fuel Quantity TOTAL LBS or FWD LBS Fuel Pressure Indicator PRESS PSI in pounds per square inch psi A red triangle represents the oil pressure limitation during a cold start shown in normal mode only Displays engine oil temperature in degrees Celsius Displays pressure of oil supplied to the transmission in pounds per square inch psi Displays the transmission oil temperature in degrees Celsius Displays the DC load in amperes to the nearest 5 amps Displays the elect
84. e 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 G1000H utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000H 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 G1000H Pilot s Guide documentation and the Bell 407GX Rotorcraft Flight Manual RFM Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G1000H 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 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B amp GARMIN __ ___ Warnings Cautions k Notes WARNING The illustrations in this guide are only examples Never use the G1000H to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo WARNING Lamp s inside this product may contain mercury HG and must be recycled or disposed of accordin
85. e reinserted PFD1 or MFD1 CARD 2 REM Card 2 was removed Reinsert card he SD card was removed from the bottom card slot of the PFD or MFD The SD card needs to be reinserted PFD1 or MFD1 CARD 1 ERR Card 1 is invalid he SD card in the top card slot of the PFD or MFD contains invalid data PFD1 or MFD1 CARD 2 ERR Card 2 is invalid he SD card in the bottom card slot of the PFD or MED contains invalid data HDG PRESET MODE Magnetic anomoly detected HPM is available he magnetometer has detected a magnetic anomoly that could affect heading indications Heading Preset Mode may be used USER MAG VAR User magnetic variation s active User magnetic variation mode was selected during previous operation and is still active checked at power up 120 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Annunciations 8 Alerts FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Results Flight plan successfully imported Description A flight plan file stored on the SD card was successfully imported as a stored flight plan File contained user waypoints only User waypoints imported successfully No stored flight plan data was modified The file stored on the SD card did not contain a fligh
86. eady displayed press the SETUP 2 Softkey Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the altitude shown in the MAX SELECTED field Turn the small FMS Knob to select the maximum altitude at which VCO alerts will be enabled from from 50 to 500 feet or select NONE to disable all VCO alerts When finished press the FMS Knob Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION A WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVS is intended as an aid to situational awareness only and may not provide the accuracy and or fidelity upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic amp WARNING Do not use SVS runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing Synthetic Vision System SVS functionality is offered as an enhancement to the G1000H Integrated Flight Deck System SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots perspective SVS information is shown on the primary flight display PFD SVS offers a three dimensional view of terrain and obstacles Terrain
87. ected a problem The system should be serviced MANIFEST PFD1 mismatch commun software ication halted MANIFEST MFD 1 software mismatch commun ication halted The PFD and or MFD has incorrect software installed The system should be serviced PFD1 CONFIG P FD1 config error Config service req d The PFD configuration settings do not match backup configuration memory The system should be serviced error Config servic MFD1 CONFIG MFD1 config e req d The MFD configuration settings do not match backup configuration memory The system should be serviced SW MISMATCH version mismatch GDU software Xtalk is off The MFD and PFD have different software versions installed The system should be serviced 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX soJnjeoJ 2 AEN Sd 24V oipny uadx svoli paezey nubi wi0 gt AeN nubi jeuonippy uoneiedo Jeuuouqy EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix eod Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES CONT A GARMIN Message PFD1 COOLING PFD1 has poor cooling Reducing power usage Comments MFD1 COOLING MFD1 has poor cool
88. ected airports These diagrams provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways ramps runways terminals and services This information should not be used by the pilot as the basis for maneuvering the aircraft on the ground This database is updated on a 56 day cycle ChartView Optional 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 Optional FliteCharts resemble the paper version of AeroNav Services terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 Press the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and press the SHW CHRT Softkey 2 Press the DP STAR
89. ements from 0 to 10096 Press the BACK Softkey to return to the previous softkey level Press the RESET Softkey to return the display to the default settings 94 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN Additional Features Input Selection With the AUX VIDEO Page displayed press the INPUT Softkey to switch between Input 1 and Input 2 Display Selection With the AUX VIDEO Page displayed press the HIDE MAP Softkey to switch between Split Screen and Full Display Zoom Range 1 Press the VID ZM or VID ZM Softkeys to increase or decrease the video display magnification between 1x and 10x 2 Use the Joystick to adjust the current displayed portion of the full display The RANGE Knob can be used to increase or decrease the range setting on the map display or zoom in and out on the video display While in the Split Screen mode pressing the MAP ACTV or VID ACTV Softkey determines which display the RANGE Knob adjusts Pressing the softkey to display MAP ACTV allows the RANGE Knob to control the range setting of the map display Pressing the softkey to display VID ACTV allows the RANGE Knob to control the zoom setting of the video display 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 95 2 Buluueld AeN Sd5 S24V olpny uqax svola siu u nnsul Tu102 AEN 346 eouepioAy paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeu
90. en the On and Off Full Screen Options 5 Turn the small FMS Knob to choose between Day Auto and Night Options 6 In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity 7 Press the FMS Knob when finished to remove the Chart Setup Menu AOPA AIRPORT DIRECTORY AOPA Airport Directory adds enhanced airport information when viewing airports on the WPT Airport Information Page This database is updated four times per year Check flygarmin com for the current database View Airport Directory Information While viewing the WPT Airport Information Page if necessary press the INFO 1 Softkey to change the softkey label to display INFO 2 AOPA airport information is displayed on the right half of the display 16 Garmin G1000H Cockpit Reference Guide for the Bell 4076X 190 01254 00 Rev B E GARMIN Features SATELLITE TELEPHONE AND DATA LINK SERVICES OPTIONAL NOTE Separate accounts must be established to access the Iridium satellite network for voice and Garmin Flight Data Services for data transmission of maintenance reports Operation of these features in the cockpit is accomplished through the AUX TELEPHONE AUX TEXT MESSAGING AUX REPORT STATUS and AUX WI FI SETUP Pages Registering the Iridium Satellite System A subscrib
91. entry point should be entered at this time Turn the small FMS Knob one click dockwise and press the LD AIRWY Softkey or press the MENU Key and select Load Airway The Select Airway Page is displayed The LD AIRWY Softkey or the Load Airway menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown first in the list followed by all altitude airways and then high altitude airways Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN ight Planning 6 Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted 7 Press the ENT Key The system returns to editing the flight plan with the new airway inserted sjuauimasu Yid 5721 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 Tum 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 olpny uqax 0105 AEN 52 AEN 540 REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT PLAN 1 Press the FPL Key to di
92. enu b Turn either FMS Knob to place the cursor on Sort By Address Press the ENT Key The sorting selection is indicated at the bottom center of the list window Viewing The Content of a Text Message 1 While viewing the AUX TEXT MESSAGING Page select the desired message box 2 Press the FMS Knob to activate the cursor 3 Turn either FMS Knob to select the desired message 4 Press the VIEW Softkey Or Press the ENT Key Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on View Selected Message Press the ENT Key 5 To close the text message press the CLOSE Softkey Or 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 87 s unp ooad Buluueld AEN 640 S24V oipny uadx sv l3 sjueumasu Wil Tuo2 NeN wb aoueplony paezey xipuaddy suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 88 A GARMIN a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Close Message Press the ENT Key Mark Selected Message As Read 1 2 3 While viewing the Inbox on the AUX TEXT MESSAGING Page press the FMS Knob to activate the c
93. er account must be established for each Tridium transceiver prior to using the Iridium Satellite System for telephone services Before setting up an Iridium account obtain the serial number of the Iridium Transceiver GSR1 and the System ID by selecting the AUX SYSTEM STATUS Page Contact Garmin Flight Data Services at 1 866 739 5687 in the United States or 913 397 8200 ext 1135 After a subscriber account has been established the system must be registered for datalink features such as reporting services or GFDS World Wide Weather Registration is accomplished by entering the required access code This process is only performed when initially setting up the system for GFDS services Registering the system for datalink services 1 With the aircraft outside and having a clear view of the sky turn the large FMS Knob on the MFD to select the AUX page group 2 Turn the small FMS Knob to select the AUX SYSTEM STATUS Note the System ID number in the AIRFRAME field 3 Tum the small FMS Knob to select the AUX REPORTS STATUS or AUX WI FI SETUP Page 4 If necessary select the REPORTS Softkey The AUX REPORT STATUS Page is now displayed 5 Press the MENU Key The Page Menu window is now displayed 6 Select Register With GFDS in the menu list 7 Press the ENT Key The Garmin Flight Data Service Registration window is now displayed 8 Enter the last four digits of the System ID number in the Access Code field 9 Press the ENT Key
94. erify stored airways This occurs when a stored flight p an contains an airway that is no longer consistent with the navigation database This alert is issued only after an navigation database update Verify use of airways in stored flight plans and reload irways as needed ab FPL TRUNC Flight plan has been truncated This occurs when a newly installed navigation database eliminates an obsolete approach or ival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach ab LOCKED FPL Cannot navigate locked flight plan This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at waypoint boxx Arriving at waypoint boox where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft will penetrate the airspace within 10 minutes ARSPC NEAR Airspace near and Special use airspace is near and ahead of the ahead aircraft position ARSPC NEAR Airspace near less than 2 nm Special
95. ert the SD card into the top card slot on the MFD Press the FPL Key to display the Active Flight Plan Page on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be exported Press the EXPORT Softkey Press the ENT Key to confirm the export Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Procedures PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Tum the large F MS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Tum the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure is active when the flight plan is active ACTIVATE A DEPARTU RE LEG 1 Press the FPL Key on the MFD to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired waypoint within the de
96. es the following Navigation Status Box fields except Active Leg TAS and DTK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD Current Track Indicator All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000H is in DR Mode HTAWS is disabled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN Amnunciations amp Alerts ANNUNCIATIONS 8 ALERTS WARNING MESSAGES See the Rotorcraft Flight Manual RFM for recommended pilot actions Annunciation Text Description Audio Alert BATTERY HO Battery overheat detected Single Chime Fire Overheat detector senses a temperature greater Continuous than or equal to 338 F Chime 0 g less than 5596 or FADEC senses engine out Continuous Fast Pulsing Chime BE oon 0 ADEC F Both the primary and reversionary channels have 1 Repeating Ding failed Dong Chime OIL PR Transmission oil pressure is low Single Chime 0 gi Transmission oil overheat is detected Single Chime CAUTION MESSAGES See the Rotorcraft Flight Manual RFM for recommended pilot actions Annunciation Text Description Audio Ale
97. ess the CAT and CAT Softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the small FMS Knob 3 Press the ENT Key Select an Available Channel within the Selected Category 1 While on the XM Radio Page press the CHNL Softkey 2 Press the CH Softkey to go up through the list in the Channel Box or move down the list with the CH Softkey Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels 3 With the desired channel highlighted press the ENT Key Entering a Channel Directly 1 While on the XM Radio Page press the CHNL Softkey 2 Press the DIR CH Softkey The channel number in the Active Channel Box is highlighted 3 Press the numbered softkeys located on the bottom of the display to directly select the desired channel number 4 Press the ENT Key to activate the selected channel 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 33 uonesado saunjeaj e uepioAy s mp oold Buruue d AEN Sd5 2 444 7218 sjueumasu unuuy jeuuouqy jeuonippy paezey bii U105 AEN ubi xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features
98. fic Map Page 1 2 68 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN avoidance 3 Press the OPERATE or NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Press the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field 5 Press the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 6 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 7 Press the FLT ID Softkey to enable or disable Flight ID displayed with the intruder information System Self Test 1 With the Traffic Map Page displayed set the range to 2 6 nm 2 Press the STANDBY Softkey 3 Press the TEST Softkey 4 Self test takes approximately eight seconds to complete When completed successfully traffic symbols are displayed and a voice alert is heard see Alerts and Annunciations section If the self test fails the system reverts to Standby Mode and a voice alert is heard Displaying Traffic on the Navigation Map 1 Ensure TAS is operating 2 With the Navigation Map displayed
99. fiers are displayed when the airport is within approximately 9 nm Resets PFD to default settings including changing units to standard Displays softkeys to select wind data parameters Headwind tailwind and crosswind arrows with numeric speed components Wind direction arrow and numeric speed Wind direction arrow with numeric direction and speed Information not displayed Displays the DME Information Window Cycles the Bearing 1 Information Window through NAVI or GPS waypoint identifier and GPS derived distance information Displays the HSI formatting softkeys Displays the HSI in a 360 degree format Displays the HSI in an arc format Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information Enables Heading Preset Mode Synchronizes heading to the selected heading Slews heading counterclockwise Slews heading clockwise Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Levell Level2 Level 3 Description 2 HPM OFF Manually disables Heading Preset Mode 5 ALT UNIT Displays softkeys for setting the altimeter and BARO settings to metric units METERS VVhen enabled displays altimeter in meters 5721 IN Press to display the BARO setting as inches of mercury olpny uqax uo2 AEN HPA Press to display the BARO setting as 2 hectopacals STD BARO Sets barometric press
100. from the call Select the HOLD Softkey again to resume the call Text Messaging SMS Messages may be sent to an email address or text message capable cellular telephone Message length is limited to 160 characters including the email address The text messaging user interface is mainly through the AUX TEXT MESSAGING Page Viewing the Text Messaging Page 1 Turn the large FMS Knob on the MFD to select the AUX page group 2 Turn the small FMS Knob to select SATELLITE PHONE 3 If necessary press the SMS Softkey to display the AUX TEXT MESSAGING Page 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX s mp o4d Buruuejd AeN Sd5 S24V olpny uqax svola siu u nnsul Tu102 AEN 346 eouepioAy paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 82 A GARMIN Message Symbol Description Received text message th ath as not been opened Received text message th ath as been opened Saved text message draft not sent System is sending text message Text message has been sent System failed to send text message Predefined text message Viewing a Text Message W
101. g to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp WARNING Because of variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners 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 reflect
102. ge CAS Display MFD 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EICAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index 4 Engine nisan 6 Crew sla ing system GARMIN CAS MESSAGE PRIORITIZATION NOTE Information on CAS messages in this pilot s guide is always superseded by the RFM Refer to the RFM for recommended pilot actions CAS messages are grouped by criticality warning caution advisory safe operating advisory and sorted by order of appearance most recent messages on top The color of the message is based on its urgency and on required action Refer to the Annunciations and Alerts section for a detailed listing of CAS alerts and alerting behavior Warning red Immediate crew awareness and immediate crew action required accompanied by one or more aural tones and a and a steady WARN PBA light is illuminated above the PFD Caution yellow Immediate crew awareness and subsequent corrective action required accompanied by a and a steady CAUT PBA light is illuminated above the PFD Advisory white Crew awareness required and subsequent action may be required Safe Operating Advisory green Crew awareness required A CAS message does not appear more than once at a given time Warning and caution CAS messages fla
103. ge the view Terrain is more than 250 ft above Red qne aircraft altitude Aircraft Altitude Terrain is between 250 ft and 0 ft Orange above the aircraft altitude Aircraft Altitude Terrain is between 0 ft and 250 ft Yellow below the aircraft altitude Aircraft Altitude Green Terrain is between 250 ft and 500 ft below the aircraft altitude Aircraft Altitude Black Terrain more than 500 ft below the aircraft altitude Terrain Altitude Color Correlation for HTAWS Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Unlighted Obstacle Hazard Avoidance Lighted Obstade lt 1000 AGL gt 1000 AGL lt 1000 AGL gt 1000 AGL Obstacle Location A A A Red obstacle s at or above current aircraft altitude A x A Yellow obstade is between 0 and 250 below current aircraft altitude A A Gray obstacle is 250 or more below current aircraft altitude HTAWS Obstacle Colors and Symbology Potential Impact Example Point Symbol 52 Annunciation X Warning X Caution TERRAIN HTAWS Potential Impact Point Symbols with Alert Types Showing hiding aviation information on the HTAWS Page 1 Press the MENU Key 2 Select Show Aviation Data or Hide Aviation Data choice dependent on current state and press the ENT Key
104. gends for Displayed GFDS Weather Products 1 Select the GFDS Weather Data Link Page 2 Select the LEGEND Softkey to display the legends for the displayed 58 weather products Garmin G1000H Cockpit Reference Guide for the Bell 4076X 190 01254 00 Rev B A GARMIN Or Hazard Avoidance a Press the MENU Key b Select Weather Legend and press the ENT Key 3 Turn the FMS Knob to scroll through the legends if more are available than fit in the window 4 Toremove the Legend Window select the LEGEND Softkey the ENT or the CLR Key or press the FMS Knob Setting Up and Customizing Weather Data for the Navigation Map Page 1 Select the Navigation Map Page 2 Press the MENU Key 3 With Map Setup highlighted press the ENT Key 4 Turn the small FMS Knob to select the Weather Group and press the ENT Key 5 Turn the large FMS Knob or press the ENT Key to scroll through product selections 6 Turn the small FMS Knob to scroll through options for each product ON OFF range settings 7 Press the ENT Key to select an option 8 Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings GFDS Weather Data Requests The GFDS Data Request window provides the flight crew with the options to define the requested weather coverage area s choose automatic weather update intervals Gf desired and the ability to send or cancel weather data requests The wind
105. hartview database error exists The MFD detected a failure in the ChartView database optional feature Ensure is properly inserted persists system should be serviced the data card Replace data card If problem MFD1 DB ERR MFD1 FliteCharts database error exists The MFD detected a failure in the FI database optional feature Ensure is properly inserted persists system should be serviced iteCharts the data card Replace data card If problem MFD1 DB ERR 1 Airport Directory database error exists system should be serviced The MFD detected a failure in the Airport Directory database Ensure that the data card is properly inserted Replace data card If problem persists the 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX saunqea4 2 Bujuuejd AEN Sd 24V oipny uadx svoli siu u n su paezey nubi nubi jeuonippy uoneiedo Jeuuouqy i ES x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS KPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Navigation database mismatch Xtalk is off Comments The PFD and MFD have different navigation database versions or regions installed Crossfill is off Check
106. hen Received When viewing MFD pages other than the AUX TEXT MESSAGING Page a pop up alert will be displayed when a new text message is received Press the VIEW Softkey to view the message Pressing the IGNORE Softkey will extinguish the pop up window and leave the text message unopened Pressing the IGNR ALL Softkey will extinguish the pop window and ignore all future incoming text messages Pressing the SMS Softkey will display the AUX TEXT MESSAGING Page The pop up alerts may be enabled or disabled through the Page Menu Enable Disable Incoming Text Message Pop Up Alerts With the AUX TEXT MESSAGING Page displayed press the MENU Key on the MFD to display the Page Menu Turn either FMS Knob to place the cursor on Disable New Message Popups or Enable New Message Popups 1 2 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN 3 Press the ENT Key The pop up alert vvill not be displayed vvhen an Additional Features incoming text message is received Reply to a Text Message While viewing the text message press the REPLY Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Reply To Message Press the ENT Key Sending a Text Message 1 While viewing the AUX TEXT MESSAGING Page press the NEW Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cur
107. iation Text Description Float system is in test mode Engine Quiet Mode is on Aircraft is on the ground 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX So1nje24 eouepioAy s mp oold Buruue d AEN Sd5 yi oipny uddx sv l3 siu umnnsu euonippv uoneiedo jJeuuouqv x pul iui nuru paezey ic EE Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS KPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix eae Annunciations amp Alerts A GARMIN HTAWS ALERTS MFD PFD HTAWS Alert Type Page Alert B Aural Message except HTAVVS Annunciation Page Reduced Required TERRAIN Waming Terrain Terrain Terrain Clearance Warning RTC Imminent Terrain TERRAIN Waming Terrain Terrain Impact Warning ITI Reduced Required OBSTACLE Warning Obstade Obstade Clearance Obstacle Warning ROC Imminent Obstacle OBSTACLE Warning Obstacle Impact Warning 101 Obstacle Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Terrain Terrain Clearance Caution RTC Imminent Terrain TERRAIN CAUTION TERRAIN Caution Terrain Terrain Impact Caution ITI Reduced Required OBSTACLE CAUTION OBSTACLE Caution Obstacle Obstacle Clearance Obstacle Caution ROC Imminent Obstacle O
108. igation APR DWNGRADE Approach downgraded Vertical guidance generated by SBAS is unavailable use LNAV only mini mums TRUE APR True north approach Change HDG reference to TRUE Displayed after passing the first true north approach when the n AUTO waypoint of a av angle is set to GPS1 SERVICE GPS1 needs A failure has been detected in the GPS1 and or Service Return unit for repair GPS2 receiver The receiver may still be available GPS2 SERVICE needs The system should be serviced service Return unit for repair NAV1 SERVICE NAV1 needs serice A failure has been detected in the NAV1 and or pair NAV2 receiver The receiver may still be available NAV2 SERVICE m z needs The system should be serviced service Return unit for repair 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 113 so1njeoJ exuepiony seinpa2oJd Buruuejg AEN 5640 2 olpny uqax svoli s u un su paezey nubi Mbi jeuonippy uoneiedo Jeuuouqy ES x pul Annunciations 8 Alerts A GARMIN GIA 63H MESSAGE ADVISORIES CONT Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Message NAV1 RMT XFR NAV1 remote transfer key is stuck
109. ighlighted 12 Press the ENT Key to activate Direct to Navigation from the PFD 1 Press the Direct to Key 2 Tum the large FMS Knob to place the cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on 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 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX sjuauimasu sub 5721 oipny uddx UI0JNeN ACN 540 S24V suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d unuuy Jeuuouqy Jeuonippy paezey n xipuaddy x pul Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EICAS GPS Nav AFCS Appendix Alerts Operation Features Avoidance Procedures Index GPS Navigation 1 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET distance field Tu
110. ight plan waypoint by one of the following 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 43 aoueplony paezey suelv uoneiedo s n e 4 Tunuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Flight Procedures Planning GPS Nav Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Appendix Alerts Operation Features Index Flight Planning A GARMIN a Enter the user waypoint identifier facility or city b 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 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 e Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 44 1 2 3 4 5 Press the FPL Key Press the FMS knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint after the desired airway entry point If this waypoint is not a valid airway entry point a valid
111. in radar scans Infrared Satellite Infrared Satellite IR SAT data depicts cloud top temperatures from satellite imagery Brighter cloud top colors indicate cooler temperatures occurring at higher altitudes D sPLAYING CLOUD Tops INFORMATION 1 Select the GFDS Weather Data Link Page 2 Select the IR SAT Softkey To display the Infrared Satellite legend select the LEGEND Softkey when Infrared Satellite data is selected for display Datalink Lightning Lightning data shows the approximate location of cloud to ground lightning strikes A strike icon represents a strike that has occurred within a two kilometer region Neither cloud to cloud nor the exact location of the lightning strike is displayed If the aircraft is also equipped with the L 3 WX 500 Stormscope only one lightning product may be enabled for display at a time D sPLAYING DarALINK LIGHTNING INFORMATION 1 Select the MAP Softkey for the PFD Inset Map select the INSET Softkey This step is not necessary on the GFDS Weather Data Link Page 2 Select the DL LTNG Softkey To display the Datalink Lightning legend on the Weather Data Link Page select the LEGEND Softkey when Datalink Lightning is selected for display SIGMETs and AIRMETs The entire SIGMET or AIRMET is displayed as long as any portion of it is occurring within the coverage area of the GFDS data request 64 Garmin G1000H Cockpit Reference Guide for the Bell 4076X 190 01254 00 Rev B A GARMIN
112. ing Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the system should be serviced Key is stuck PFD1 KEYSTK PFD1 key name Key is stuck MFD1 KEYSTK MFD key name problem persists 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 CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage serviced The PFD1 voltage is low The system should be MFD1 VOLTAGE MFD1 has low voltage Reducing power usage serviced The MFD voltage is low The system should be DATABASE MESSAGE ADVISORIES Message Comments MFD1 DB ERR MFD1 navigation The MFD and or PFD detected a failure in the database error exists navigation database Attempt to reload the PFD1 ERR PFD1 navigation navigation database If problem persists the database error exists system should be serviced MFD1 DB ERR MFD1 basemap database error exists The MFD and or PFD detected a failure in the PFD1 DB ERR PFD1 basemap basemap database database error exists MFD1 DB ERR MFD1 terrain The MFD and or PFD detected a failure in the database error exists terrain
113. io Panel Pressing the NAVI or NAV2 Key selects and deselects the navigation radio source Selected audio can be heard over the headset and the speaker if selected All radios can be selected individually or simultaneously Selecting a NAV Radio Receiver NAV COM TUNING 1 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned 2 Tum the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz 3 Press the Frequency Transfer Key to place the frequency into the active frequency field 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX sjueauinajsu nubi S24V oipny uadx sv l3 JUI05 AEN Suelv uoneiado SoJnjeaJ aoueplony 4 Fuluueld AEN Sd5 unuuy jeuuouqy jeuonippy paezey Wia x pu ddy x pul Nav Com AFCS XPDR Audio EICAS Abnormal Additional Hazard Annun Flight Instruments Flight Planning GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN DIGITAL CLEARANCE RECORDER AND PLAYER OPTIONAL The Audio Panel contains a digital clearance recorder that records up to 2 5 minutes of the selected COM radio signal Recorded COM audio is stored in separate memory blocks Once 2 5 minutes of recording time have been reached the recorder begins
114. ion Vleather Product Symbol q EIER S Minutes Minutes GE Aerodrome Reports ni ratas mue The composite precipitation image is updated every 3 minutes but individual radar sites may take between 3 and 10 minutes to provide new data Setting Up and Customizing the GFDS Weather Data Link Page 1 2 3 4 5 6 7 8 Select the GFDS Weather Data Link Page Press the MENU Key With Weather Setup highlighted press the ENT Key Turn the small FMS Knob to select Product Group 1 or Product Group 2 and press the ENT Key Turn the large FMS Knob or press the ENT Key to scroll through product selections Turn the small FMS Knob to scroll through options for each product ON OFF range settings etc Press the ENT Key to select an option Press the FMS Knob or CLR Key to return to the GFDS Weather Data Link Page with the changed settings On aircraft equipped with both GFDS and XM WX Satellite Weather services customizing the display settings for the corresponding weather products shown in following table will result in identical settings for both services XM Weather Product GFDS Worldwide Weather Product Next generation Radar Precipitation NEXRAD PRECIP Cloud Top Infrared Satellite CLD TOP IR SAT 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 57 AEN Sd5 S24V oipny duadx 59213 sjueumnsu u102 AEN
115. ion volume up of desired increased z selection g Decreases Desired selection volume volume Volume of desired selection Sz ms Volume down of desired decreased P Adjustments sledon ge NOTE Finer volume adjustment may be made using the dual concentric knobs 5 on the GMA 350H The voice command Up or Down is equivalent to three a click of the inner knob Desired selection speaker pilot copilot passenger pass 2 marker aux auxiliary telephone phone jack or music Voice Response ji i Enables 3D p Three D audio Three D audio left three D Sz audio 5 Ja audio right 82 30 Audio Enables i standa rd Voice Response 2 Standard audio audio Standard Audio 5 disables 30 audio T Voice Recognition Commands gm ge xipuaddy suelv uoneiedo yunuuy jeuuouqy x pul 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 21 GARMIN Nav Com XPDR Audio Panel Sjueuinijsu fila 5721 oipny uadx 52 AeN 549 Buluuejd r Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 4076X 28 A GARMIN AUTOMATIC FLIGHT CONTROL SYSTEM Not available 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX AFCS 29
116. is to be used to calculate vertical guidance perform the following steps a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to highlight the desired waypoint altitude Press the ENT Key to designate the altitude for use in giving vertical guidance ACTIVATE AN ARRIVAL LEG 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired waypoint within the arrival Press 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 1 2 50 NOTE If certain GPS parameters SBAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN 5 Press the ENT Key A list of available approaches for the destination airport is displayed 4 Turn either FMS Knob to highlight the desired approach 5 Press the ENT Key A list of available transitions for the selected approach procedure is now displayed 6 Turn either FMS Knob to select the desired transition The Vectors option assumes vectors wi
117. isplay the Page Menu b Turn either FMS Knob to place the cursor on Show Draft Messages Press the ENT Key The message box selected for viewing is indicated at the bottom left of the list window Arranging Text Messages The viewed messages may be listed according to the date time the message was sent or received the type of message read unread sent unsent etc or by message address 86 View Messages Sorted by Message Date Time While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the TIME Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Sort By Date Time Press the ENT Key The sorting selection is indicated at the bottom center of the list window Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Additional Features View Messages Sorted by Message Type While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the TYPE Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Sort By Type Press the ENT Key The sorting selection is indicated at the bottom center of the list window View Messages Sorted by Address While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the ADDRESS Softkey Or a Press the MENU Key to display the Page M
118. ive coatings CAUTION The Garmin G1000H 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 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Wamings Cautions amp Notes 5 GARMIN NOTE All visual depictions contained within this document including screen images of the G1000H panel and displays are subject to change and may not reflect the most current G1000H system and aviation databases Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data 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 6
119. l 407GX Index Index 3 sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 S24JV oipny uddx sY213 sjuaumasu jeuonippy 2 nubi Tuo2 NeN wb uoneiedo Jeuuouqy Sue v unuuy 1221 ow GARMIN index Sjueuinijsu fila 5721 Tu102 AEN s24v AeN Sd5 buluueld Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy WA ES 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Index 4 A GARMIN Garin International Inc 1200 East 151st Street r o Olathe KS 66062 USA m p 913 397 8200 f 913 397 8282 Or i 4 3 g h mya Garmin AT Ind aa ess 2 2345 Turner Road SE r a 777 alem OR 97302 USA T a 033642138 a 2011 Garmin ltd or its subsidiaries 190 01254 00 Rev B
120. le The system should be serviced Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Annunciations 8 Alerts GMA 350H MESSAGE ADVISORIES CONT Message GMA1 CONFIG GMAT config error Config service req d Comments The audio panel configuration settings do not match backup configuration memory The system should be serviced MANIFEST GMAT software mismatch communication halted The audio panel has incorrect software installed The system should be serviced GMAT SERVICE GMAT needs Service Return unit for repair The audio panel self test has detected a problem n the unit Certain audio functions may still be vailable and the audio panel may still be usable he system should be serviced when possible m GIA 63H MESSAGE ADVISORIES Message GIA1 CONFIG GIA1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d Comments The GIA1 and or GIA2 configuration settings do not match backup configuration memory The system should be serviced GIA1 CONFIG GIA1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d The GIA1 and or GIA2 have an error in the audio configuration The system should be serviced GIA1 COOLING GIA1 temperature m d k The GIA1 and or GIA2
121. ll be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO UJ 9 Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected approach oipny uddx Sy2l3 siu u nnsu ui UI0JNeN 52 AEN 540 procedure 10 Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted 11 Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and activates the first leg of the approach 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 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Duruue d wold s mp old eouepioAy paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com
122. ls may be used manually to control the GMA 350H The following table lists the available Voice Recognition commands the associated actions and the voice response if applicable 22 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Nav Com XPDR Audio Panel SjueuinJjsu iui S24V oipny 4ddX svo JUI05 AEN AEN Sd5 Duruue d LITE SoJnpa0Jd eouepioAy paezey saunqee4 jeuonippy uoneiedo Jeuuouqy Sue v unuuy xipueddy Control Spoken Command Action Confirmation of Action 7 Toggles Illuminate Extinguish COM1 COM ane COM Annunciator MIC one Selects MIC1 Illuminate MIC1 Annunciator COM one MIC u i Toggles luminate Extinguish COM2 0 2 Annunciator MIC two Selects MIC2 Illuminate MIC2 Annunciator COM two MIC Toggles Illuminate Extinguish COM3 COM ihres COM3 Annunciator MIC three Selects MIC3 Illuminate MIC3 Annunciator COM three MIC ak Selects split uminate MIC1 MIC2 COM 1 2 Annunciators cul i Selects split uminate MIC1 MIC2 COM COM 1 2 Annunciators a i Selects split uminate MIC1 MIC3 o COM 1 3 Annunciators cul Selects split uminate MIC2 MIC3 COM 2 3 Annunciators utes monitored Monitored COM mute or COM on Voice Response Mute monitored COM primary
123. n Index Appendix Annunciations 8 Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message FAILED PATH A data path has failed Comments A data path connected to the GDU or the GIA 63H has failed MAG VAR WARN Large magnetic variance Verify all course angles The GDU s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may differ from the actual magnetic heading by more than 2 SVS SVS DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVS SVS DISABLED Terrain DB resolution too low 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 CHECK CRS Database course for LOC1 LOC ID is CRS Selected course for LOC1 differs from published localizer course by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS Selected course for LOC2 differs from published localizer course by more than 10 degrees PFD1 or MFD1 CARD 1 REM Card 1 was removed Reinsert card The SD card was removed from the top card slot of the PFD or MFD The SD card needs to b
124. n and consequently the system may display a path that is different than the actual movement of the aircraft Estimated position information displayed by the G1000H through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS SBAS Mode due to the lack of satellite measurements needed to determine a position Changes in wind speed and or wind direction compounds the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness using other navigation equipment until GPS derived position data is restored 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 99 sampaod uluueld AEN 540 52 oipny uadx svo syuoumasul uo2 AEN paezey saunyea4 Jeuonippy Sue v unuuy xipueddy x pul iui bi Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Annun EICAS AFCS Alerts Features Procedures GPS Nav Appendix Index Abnormal Operation 100 A GARMIN CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includ
125. n for each display Loading the Jeppesen Navigation Database as the Standby Navigation Database NOTE After the navigation database is loaded or copied the top SD card may be removed 1 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD 2 Verify that an SD card is inserted in the bottom slot of each PFD and the MFD 3 Turn the system ON A prompt is displayed 4 Press the YES Softkey The navigation database is copied to the SD card in the bottom card slot of the MFD 5 After the navigation database files are copied to the bottom SD card press any key to continue as instructed 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX s n e 4 eouepioAy 2 buluueld AEN Sd5 24JV olpny uqax SV2l3 sjuauimasu jeuonippy 2 wold JUI0 NEN yub uoneiedo Jeuuouqy Sue v unuuy im bea Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN 6 7 8 9 10 11 12 13 14 15 16 17 18 Again press any key to continue as instructed on the display Press the NO Softkey The display now starts in normal mode Since the database effective date is not yet valid it should not be loaded as the active database The
126. n squelch volume up Manual Manual squelch threshold Squelch down or R Manual sguelch volume down 5777 ual squ I manual Manual sguelch threshold sguelch decreased Man squelch 77 down threshold NOTE Finer manual squelch adjustment may be made using the dual concentric knobs on the GMA 350H The voice command Up or Down is equivalent to three dicks of the inner knob or any combination of pilot copilot passenger or pass Plays recorded COM Play or dearance i audio refer Clearance Read back or Recorded audio playing rl r nc a to Clearance ay again Recorder section for details Distribute telephone to desired position s or Distributes Distribute phone to desired TEL JACK audio heard at position s or to desired desired position s Distribute jack to desired positions Distribution position s Blue Mode Distributes Distribute music to desired MUSIC to MUSIC heard at desired position s desired position s position s Desired position s All none pilot copilot passenger pass 26 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Nav Com XPDR Audio Panel Control Spoken Command Action Confirmation of Action 2 Increases an Aa Tae volume Volume of desired selection Desired select
127. nd 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 GEO LIMITS AHRS1 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 GMU 44 MESSAGE ADVISORIES Message Comments HDG FAULT AHRS1 magnetometer fault has occurred A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000H system should be serviced MANIFEST GMU1 software mismatch communication halted The GMU 44 has incorrect software installed The G1000H system should be serviced 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX saunjeaj s mp oold Buruue d AEN Sd5 2 oipny uddx sv l3 siu umnnsu paezey nubi Wil jeuonippy uoneiedo Jeuuouqy ie E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts GSR 56H MESSAGE ADVIS
128. nts Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EICAS Procedures Appendix Alerts Operation Features Index A GARMIN Altitudes associated with approach procedures are auto designated This means the system automatically uses the altitudes loaded with the approach for giving vertical flight path guidance outside the FAF Note these altitudes are displayed as small light blue text Altitudes associated with arrival procedures are manually designated This means the system does not use the altitudes loaded with the arrival for giving vertical flight path guidance until designated to do so by the pilot Note that these altitudes are initially displayed as white text These altitudes may be designated by placing the cursor over the desired altitude and pressing the ENT Key After designation the text changes to light blue Altitudes that have been designated for use in vertical 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 vertical flight path 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 GPS Navigation 34 to be used in determining vertical flight path guidance Altitude has been retrie
129. o return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts it may be necessary to carry another source of charts on board the aircraft SafeTaxi Optional SafeTaxi gives greater map detail as the map range is adjusted in on the airport The airport display on the map reveals runways with numbers taxivvays identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing Pressing the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Pressing the DCLTR Softkey twice removes VOR station ID the VOR symbol and intersection names if within the airport plan view Pressing n Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN Additional Features the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Pressing the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for sel
130. oading Garmin Database Updates 1 2 3 4 5 6 1 8 9 10 11 12 VVith system povver OFF remove the MFD database card from the bottom card slot of the MFD Update the Garmin databases on the MFD card Insert the MFD database card into the bottom card slot of the MFD Apply power to the system check that the databases are initialized and displayed on the power up screen When updating the terrain and FliteCharts databases a Verifying message may be seen If this message is present wait for the system to finish loading before proceeding to step 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete being displayed Remove and reapply power to the system Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show database information for each display MFD1 DB PFD1 DB Verify the correct database cycle information is shown for each database for each display Loading the Jeppesen Navigation Database as the Active Navigation Database NOTE Loading the Jeppesen navigation database as the active database pri
131. on Inset Map optional Displays METAR flags on airport symbols shown on the Navigation Map Displays the legend for the selected weather products Available only when NEXRAD XM LTNG and or METAR softkeys are selected Returns to top level softkeys Selects desired amount of map detail cycles through declutter levels DCLIR 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 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Appendix Level 1 Level 2 Level 3 Description SHW CHRT CHKLIST When available displays optional airport and terminal procedure charts When available displays optional checklists LOADING UPDATED DATABASES Ay CAUTION Never disconnect power to the system when loading a database Power interuption during the database loading process could result in main tenance being required to reboot the system NOTE When loading database updates the DB Mismatch message will be displayed until database synchronization is complete followed by turning system power off then on Synchronization can be monitored on the AUX SYSTEM STATUS Page In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional It may also be necessary to have the system
132. onfiguration for the power assurance check is invalid the error message CHK LIMITS is displayed Otherwise the power assurance check will complete after ten seconds Values that equal or exceed performance minimums will be displayed in white values that do not meet performance minimums will be shown with yellow highlighted black readouts Dashes are displayed if data used to perform the power assurance check is not available 8 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN CREW ALERTING SYSTEM CAS When Crew Alerting System CAS messages are generated a CAS window containing messages appears to the right of the vertical speed indicator on the PFD Pressing the CAS Softkey displays softkeys for scrolling up and down through the messages in the PFD CAS Window PFD CAS Window CAS Scrollin Softkey Enable when more than 12 messages are displayed N CDI OE CAS Display PFD CAS alerts are additionally displayed on the upper left of the EIS Engine page Up to 19 messages can be shown when more than 19 messages accumulate the CAS and CASV Softkeys will become available as needed to permit scrolling up and down through the messages on this page manif 11 55 111 90 TPH m o 136 975 1122 900 con m BP 215 ETE 136 975 cree MED Alerts window containing CAS messages CAS Scrolling Softkeys Enabled when more than 19 messages are displayed PUR OK Engine Pa
133. or to its effective date will result in the expiration date on the power up screen and the effective date on the AUX System Status Page being displayed in yellow NOTE After the navigation database is loaded or copied the top SD card may be removed Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Appendix 1 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the display PFD or MFD to be updated label of SD card facing left 2 Turn the system ON A prompt is displayed in the upper left corner of the display 3 Pressthe NO Softkey to proceed to loading the active database 4 Aprompt similar to the following is displayed Press the YES Softkey to update the active navigation database 5 After the update completes the display starts in normal mode 6 Turn the system OFF and remove the SD card from the top card slot 7 Repeat steps 1 through 6 for the other displays PFD or MFD 8 Apply power to the system and press the ENT Key to acknowledge the startup Screen 9 Turn the large FMS Knob to select the AUX Page group on the MFD 10 11 Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show active navigation database information for each display MFD1 DB PFD1 DB Verify the correct active navigation database cycle information is show
134. ow also displays the status of the GFDS data request process Requesting GFDS Weather Data Manually 1 Select the GFDS Weather Data Link Page 2 Press the MENU Key 3 With GFDS Weather Request highlighted press the ENT Key 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 59 AEN Sd5 S24V oipny uddx 5219 sjuauimasu Tuo2 AEN 3 biu Duruue d nubi aoueploay s mp oold paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 4 Turn the large FMS Knob to highlight the desired coverage option s and press the ENT Key to check or uncheck one of more of the following coverage selections e PRESENT POSITION Requests data based on current location DESTINATION Requests data based on active flight plan destination if the flight plan contains no destination dashes are displayed FPL Requests data based on active flight plan Turn the small FMS Knob to select the desired flight plan look ahead distance option or choose REMAINING FPL to request the remainder of the flight plan WAYPOINT Requests data based on any valid waypoint 5 Turn the large FMS Knob highlight to the DIAMETER RTE WIDTH distance field
135. p DCLTR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan WX LGND Displays icon and age on the Inset Map for the selected weather products optional TRAFFIC Displays traffic information on Inset Map TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Inset Map NEXRAD Displays NEXRAD weather and coverage information on Inset Map optional PRECIP Displays Worldwide Weather precipitation on Inset Map optional XM LING Displays XM lightning information on Inset br Map optional DL ITNG Displays VVorldvvide VVeather lightning information on Inset Map optional METAR Displays METAR flags on airport symbols shown on the Inset Map optional 124 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Appendix optional eas ee ee ee wes L wee nn rs nynnmunnnu sjuauimasu nubi n n m 8 z Y wu Eee Press the BACK Softkey to return to the top level softkeys BRG1 GPS BRG GPS olpny uqax uo2 AEN 11 11 11 lhos sync Hos os HPM OFF Back L JL IL L jp ow gps L se E V3 V3 V3 P3 EN EN EN EN n n9 w 52 AEN 540 l l l 1 L
136. p Page as shown in the following figure Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN 0000 Appendir GRS MV DB Update Available Update from 2005 to 2010 GRS Magnetic Field Variation Database Update Prompt Loading the magnetic field variation database update With OK highlighted as shown in the previous figure press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure Uploading GRS Mag Var Database STARTING UPLOAD 0 07 Uploading Database to GRS When the upload is complete the system is ready for use 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX so1njeoJ 2 Buruuejg AEN Sd5 24V oipny uadx svoli siu un sul Jeuonippy paezey ni UI05JNeN Wila uoneiedo Jeuuouqy Sue v unuuy k GARMIN Appendix Sjueuinijsu fila 5721 oipny uadx U105 AEN s24v AeN Sd5 buluueld r Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 4076X 136 A GARMIN Symbols 3D Audio 20 A Access code 77 78 Activate a flight plan 32 Active Channel 93 Active database 133 Active Navigation Database 132 ADF 11 98 AHRS 115 Airport Signs 73 74 Airways 130 ALT 69 Altitude mode 6
137. parture 4 Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 49 sjueuimasu sub 5721 olpny uqax 0105 AEN 52 AEN 540 Duruue d nubi s mp old eouepioAy paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures GARMIN 4 5 6 7 8 9 10 11 12 Turn the large FMS Knob to highlight the desired arrival Press the ENT Key A list of transitions is displayed for the selected arrival Turn either FMS Knob to select the desired transition Press the ENT Key A list of runways may be displayed for the selected arrival Turn the large FMS Knob to highlight the desired runway Press the ENT Key VVith LOAD highlighted press the ENT Key The arrival becomes part of the active flight plan If an altitude associated with a waypoint in an arrival procedure
138. play planning data for the remainder of the flight plan NOTE The page mode must be set to MANUAL to perform the following steps 5 Turn the large FMS Knob to highlight the departure time DEP TIME field 36 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 G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Flight Planning 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 7 The flashing cursor moves to the ground speed GS field Enter the ground speed Press the ENT Key when finished Note that in automatic page mode ground speed is provided by the system 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 9 The flashing cursor moves to the fuel onboard field Enter the fuel onboard Press the ENT Key when finished Note that in AUTOMATIC page mode fuel onboard is prov 10 ided by the fuel totalizer 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 1
139. played in the Crew Alerting System Display to warrant scrolling H CAS Scroll down Displayed only when a sufficient number of items are displayed e in the Crew Alerting System Display to 22 warrant scrolling PWR CHK Displays fuel system softkeys ez MAP Enables second level Navigation Map F softkeys TRAFFIC Displays traffic information on BE Navigation Map Ss TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map gt k 5 o Fl a x x pul 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Additional Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix A GARMIN Level 1 Level 2 Level 3 Description DCLTR AIRWAYS NEXRAD or PRECIP XM LING or DL LING METAR LEGEND BACK Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed Displays NEXRAD weather and coverage information on Inset Map optional Displays Worldwide Weather precipitation on Inset Map optional Displays XM lightning information on Inset Map optional Displays Worldwide Weather lightning information
140. ptional cc ccccccssscsssssssssscssssssssssscessssssssscesssssssssscesssssssssecesssssssensess Enter a Transponder Code sss Selecting a COM Radio Selecting a NAVRAdIO wwwwww aterrar rnrn ar rent 2 NAV COM TUNINJI iii 3 Digital Clearance Recorder and Player 4 Intercom Volume and SgUelCh wwwwww 4 Intercom Modes treaties e n LER 5 Passenger Address Mode PA Mode 9 Split PA Mode iori remp ree tnter pret treo cet m S n 20 BD Audio sse nnne 20 Enabling 3D Audio wwwwwww nennen 20 3D Audio Troubleshooting seen 20 Voice Recognition tr cn tht cci Fen P ted Fe rh bn 22 AUTOMATIC FLIGHT CONTROL 5 29 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Table of Contents GARMI N GPS NAVIGATION ea a eer 31 Direct to nnne 31 Activate a Stored Flight Plan 32 Activate a Flight Plan Leg Stop Navigating a Flight Plan 33 Vertical Navigation VNAV l l s s s s s s s s s il 33 FLIGHT PLANNING Weight Planning Trip Planning entre e bre aaa Create a User Waypoint Defined by Latitude amp Longitude Create a User Waypoint Defined by Radials from Other W
141. py of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided that such electronic or pr notice and provided furthe revisi inted copy of this manual or revision must contain the complete text of this copyright hat any unauthorized commercial distribution of this manual or any on hereto is strictly prohibited ot Garmin and G1000H are registered trademarks of Garmin Ltd or its subsidiaries WATCH FliteCharts and SafeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin NavData is a registered trademark of Jeppesen Inc Stormscope and SkyWatch are regis atel tered trademarks of 1 3 Communications and XM is a registered trademark of SiriusKM ite Radio nc AOPA Membership Publications Inc and its related organizations hereinafter collectively AOPA expressly disclaim all warranties with respect to the AOPA information included in this data and fitness for a particular purpose The in express or implied including but not limited to the implied warranties of merchantability formation is provided as is and AOPA does not warrant or make any representations regarding its accuracy reliability or otherwise Under no circumstances induding negligence shall AOPA be liable for any incidental
142. radio Pressing the CDI Softkey a third time activates GPS mode Pressing the CDI Softkey again cycles back to NAVI While cycling through the CDI Softkey selections the NAV Tuning Box and the Frequency Transfer Arrow are placed in the active NAV Frequency Field and the active NAV frequency color changes to green The three navigation modes that can be cycled through are e VORI or LOCI If NAVI is selected a green single line arrow not shown labeled either VORI or LOCI is displayed on the HSI and the active NAVI frequency is displayed in green VOR2 or LOC2 If NAV2 is selected a green double line arrow shown labeled either VOR2 or LOC2 is displayed on the HSI and the active NAV2 frequency is displayed in green GPS If GPS Mode is selected a magenta single line arrow not shown appears on the HSI and neither NAV radio is selected Both active NAV frequencies are then displayed in white Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Nav Com XPDR Audio Panel Standby Active Fields Fields NAV1 117 88 nav2 113 25 lt Tuning Box The NAV Radio is Selected by Pressing the CDI Softkey Selecting a NAV Radio for Navigation See the Flight Instruments Section for selecting the DME optional and Bearing Information windows and using VOR as the source for the bearing pointer NAV radios are selected for listening by pressing the corresponding keys on the Aud
143. ransmission of data packets less than 300 bytes Wi Fi is used only when the aircraft on the ground and the system is connected to a Wi Fi network 4 Press the ENT Key Enabling disabling Automatic Send for Automatic Test Reports 1 While viewing the Report Status Page press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to move the cursor to the AUTOMATIC SEND field 3 Turn the small FMS Knob to select ENABLED or DISABLED 4 Press the ENT Key Enabling disabling Periodic Send for Periodic Test Reports 1 While viewing the Report Status Page press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to move the cursor to the PERIODIC SEND field 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 21 xipuaddy suelv uoneiedo sainjea4 aoueplony SoJnpa20Jd Duruue d AEN Sd5 S24JV oipny uddx SV2l3 junuuy Jeuuouqy Jeuonippy p EzeH ubi u102 AEN x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 3 4 A GARMIN Turn the small FMS Knob to select ENABLED or DISABLED Press the ENT Key Sending a Transmission Manually 1 2 3 1 2 3 4 5 6 NOTE Manual transmission of data can only be performed while the aircraft is on the ground While viewing the Report Stat
144. ration Proximity Advisory PA Not available with TIS system intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory TA dosing rate distance and vertical separation meet TA criteria Traffic Advisory TA arrow with ADS B directional info the direction of t Traffic Advisory Off Scale he intruder aircraft track GTS 800 only mation Points in Proximity Advisory PA arrow with ADS B directional information Points in the direction of t he aircraft track GTS 800 only Non threat traffic arrow with ADS B directional information Poi direction of the intruder aircraft track GTS 800 only nts in the 190 01254 00 PA or Non threat traffic arrow with ADS B directional informatio positional accuracy is degraded Points in the direction of the ai GTS 800 only Traffic Symbol Description Garmin G10 00H Cockpit Reference Guide for the Bell 407GX n but rcraft track 67 AEN Sd5 S 24V oipny uddx 5219 sjuauimasu Tuo2 AEN PULTE Duruue d nubi s mp oold paezey suelv uoneiedo sainjea4 junuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance
145. recording over the stored memory blocks starting from the oldest block An optional external Play button controls the play function Pressing the Play button once plays the latest recorded memory block Pressing the MKR MUTE Key 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 optional Play button while audio is playing begins playing the previously recorded memory block Each subsequent press of the Play button selects the previously recorded memory block Powering off the unit automatically clears all recorded blocks INTERCOM VOLUME AND SQUELCH The VOL CRSR Knob controls selection and volume or manual intercom squelch adjustment for audio sources that may not be adjustable anywhere else in the system The small knob controls the volume or squelch Turning the large knob activates and or moves the cursor flashing green annunciator or flashing blue annunciator in Blue Select Mode to select the audio source to adjust The cursor will time out after a few seconds and the position of the cursor will always default back to the PILOT Key Pressing the small knob cancels the cursor Manual Squelch Annunciator Off for Automatic Squelch On for Manual Relative Volume Squelch Squelch Scale GARMIN GMA 350 Cursor Volume or Manual Squelch Volume Squelch Control Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B
146. rical bus voltage Displays the usable fuel quantity in pounds By default total usable fuel quantity is shown when forward fuel tank is selected FWD is displayed above readout to indicate forward tank usable fuel quantity is shown Displays fuel pressure in pounds per square inch psi Total Fuel Quantity Displays total usable fuel quantity as a bar Gauge graph Fuel Flow Indicator Displays fuel flow in pounds per hour PPH FF PPH Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Engine Indication S Crew Alerting System ENGINE POWER AND SPEED INDICATIONS Box Indicates Parameter Controlling PSI Indicator Maximum Continuous Power Operation Limit Torque Readout MGT Readout NGR Power Available Gauge G Readout NR Indicator Power Available Indicator NP Indicator Dual Tachometer Gauge Power Situation Indicator Gauge and Dual Tachometer Gauge Power Situation Indicator The PSI provides the pilot with the amount of power available based on engine torque Q shown as a percentage measured gas temperature MGT degrees Celsius C and gas producer rotation speeds NG shown as a percentage with respect to operating limitations In normal conditions a green box is shown around the label for the readout currently closest to its maximum continuous power MCP limits This value also controls a green pointer along a numeric scale from 0 no power to 10
147. rmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN 3D Audio Troubleshooting Symptom s Solution s 3D audio left message heard in both ears 3D audio right message not heard 3D audio left message heard in both ears followed by 3D audio right message heard in both ears 3D audio right message heard in both ears 3D audio left not heard 3D audio left message heard in right ear only followed by 3D audio right message heard in left ear only 190 01254 00 Rev B 2 Stereo headset in use with mono stereo switch set to mono 3 Aircraft wiring has left audio wired to both left and right channels of Stereo headset jack 2 Stereo headset in use with mono stereo switch set to mono 3 Incorrect aircraft wiring left right shorted together 1 Incorrect aircraft wiring right channel used for mono instead of left or left right swapped 1 Stereo headset is on backwards 2 Incorrect aircraft wiring left right channels swapped Nav Com XPDR Audio Panel 2 3 2 3 1 1 2 Set mono stereo switch on headset to stereo If after checking solutions 1 and 2 see a service center as soon as possible to inspect correct wiring This wiring fault can cause fail safe audio not to function 1 Mono headset in use 1 Use a stereo headset Set mono stereo switch on headset to stereo If after checking solutions
148. rn 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 MFD and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Press the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 32 1 2 3 4 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint Press the ACT LEG Softkey on the MFD OR Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN STOP NAVIGATING A FLIGHT PLAN GPS Naviga
149. rt Baggage door is not securely latched Battery relay energized when battery switch is off Battery still connected to DC bus Chip detector has detected debris in engine oil FADEC fault detected that may result in degraded engine performance Single Ping A fault is recorded in the FADEC FADEC is in manual operating mode Floats Arm switch is in the armed position External fuel filter is partially blocked before impending bypass 101 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX sainjea4 2 Duruue d AEN Sd5 S241V olpny uqax sY213 sjuaumasu 2 Wil uio AeN Yid jeuonippv uoneiedo jJeuuouqv EY x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts GARMIN Annunciation Text Description Audio Alert Fuel feed tank sensor indicates low fuel 100 10 pounds of fuel remain in aft tank om Fuel valve is in transition or is not in the commanded position Generator not connected to DC bus o An over temperature condition has been detected either under the pilot s seat copilot s seat or in the vertical tunnel Low pressure in hydraulic system Left fuel boost pump has failed Left fuel transfer pump has failed Litter door
150. sage box may be viewed separately or together in any combination Show Inbox Messages While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the INBOX Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Show Inbox Messages Press the ENT Key The message box selected for viewing is indicated at the bottom left of the list window 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 85 xipuaddy suelv uoneiedo sainjea4 aoueplony SoJnpa20Jd buluueld AEN Sd5 S24JV oipny uddx SV2l3 sjuauimasu junuuy Jeuuouqy Jeuonippy p EzeH ubi wo gt AeN ubiu x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features A GARMIN Show Outbox Messages While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the OUTBOX Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Show Outbox Messages Press the ENT Key The message box selected for viewing is indicated at the bottom left of the list window Show Draft Messages While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the DRAFTS Softkey Or a Press the MENU Key to d
151. sages will appear in the request status window as shown in the following table 60 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Hazard Avoidance Weather Request Status Message Description Auto requests inhibited Send manual request to reset The system has disabled automatic weather data requests due to excessive errors Automatic weather data requests have stopped Send a manual weather data request to resume automatic updates Auto update retry Seconds The system will attempt another automatic weather data request after an error occurred during the previous request Timer counts down until the next automatic request occurs GFDS Comm Error 2 A communications error has occurred with the GIA The system should be serviced GFDS Comm Error 4 This occurs if multiple automatic weather data requests have recently failed or the GDL 59 or a GIA is off line GFDS Comm Error 5 The Iridium or GFDS networks are not accessible Check Iridium signal strength If this error persists the G1000H should be serviced GFDS Comm Error 6 A communications error has occurred It this error persists the system should be serviced GFDS Comm Error 7 A weather data transfer has timed out Check Iridium signal strength and re send the data request GFDS Comm Error 8 A server error has occurred or invalid data received GFDS Login Inv
152. sh when they are generated and continue to flash until acknowledged or until the triggered condition is inactive for more than 3 seconds Advisory CAS messages are displayed steady until the triggered condition is inactive for more than 3 seconds After the acknowledgment a message remains displayed at the top of its respective priority group in the CAS Window until either a newer message of the same priority appears or the condition s that caused the alert to display no longer exist Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN NavtomxPDRinudio Panel NAV COM TRANSPONDER AUDIO PANEL ADF TUNING OPTIONAL Tune the ADF using the remote ADF control head DME TUNING OPTIONAL 1 Press the DME Softkey 2 Turn the large FMS to select the DME source field 3 Turn the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection ENTER A TRANSPONDER CODE 1 Press the XPDR Softkey to display the transponder mode selection softkeys 2 Press the CODE Softkey to display the transponder code selection softkeys for digit entry 3 Press the digit softkeys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active SELECTING A COM RADIO The COM
153. sic 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 Entering Fuel Parameters 1 If necessary press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to place the cursor in the FUEL ON BOARD field 3 Press the FOB SYNC Softkey to enter the fuel on board quantity as read from the fuel quantity sensors Or Manually enter the desired fuel quantity 4 Press the ENT Key The cursor is now in the FUEL RESERVES field 5 Enter the desired reserve fuel quantity 6 Press the FMS Knob to remove the cursor TRIP PLANNING 1 Turn the large FMS Knob 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 press the AUTO or MANUAL Softkey 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 35 sjuauimasu nubi 5721 oipny uddx JUI0JNeN S24V 2 Buluuejd AEN Sd5 nubi eouepioAy paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Fligh
154. sor on Draft New Message Press the ENT Key 2 TheTEXT MESSAGE DRAFT Window is now displayed with the cursor in the TO field Enter the desired telephone number or email address Entry can be accomplished through the FMS Knob and softkeys on the MFD The FMS Knob is used to enter letters and numbers or numbers can be entered from the MFD by pressing the NUMBERS Softkey Press the CAP LOCK Softkey to create upper and lower case alpha characters Special characters can be accessed by pressing the SYMBOLS Softkey 3 Press the ENT Key The cursor is now displayed in the MESSAGE field 4 Enter the desired message using any combination of entry methods as described in step 2 5 Press the ENT Key 6 Press the SEND Softkey to send the message immediately or press the SAVE Softkey to save the message in Outbox for sending at a later time Press the CANCEL Softkey to delete the message 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 83 xipuaddy spay uoneiedo sainjea4 aoueplony saunpad0ld buluueld AEN Sd5 S24JV olpny uqax SV2l3 sjuauimasu junuuy Jeuuouqy Jeuonippy p EzeH ubi u05 AeN ubiu x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 84 A GARMIN Predefined Text Messages Time an
155. splay the Page Menu Turn either FMS Knob to place the cursor on Stop Editing Predefined Message Press the ENT Key Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Additional Features Send a Predefined Text Message 1 While viewing the AUX TEXT MESSAGING Page press the NEW Softkey 2 TheTEXT MESSAGE DRAFT Window is now displayed with the cursor in the TO field Enter the desired telephone number or email address Entry can be accomplished through the FMS Knob and softkeys on the MFD The FMS Knob is used to enter letters and numbers or numbers can be entered from the MFD by pressing the NUMBERS Softkey Press the CAP LOCK Softkey to create upper and lower case alpha characters Special characters can be accessed by pressing the SYMBOLS Softkey 3 Press the ENT Key The cursor is now displayed in the MESSAGE field 4 Press the PREDEFD Softkey The PREDEFINED MESSAGE MENU Window is displayed 6 Press the ENT Key The predefined message text is inserted into the message field If desired the message can be edited by using the FMS Knobs 7 Press the ENT Key 8 Press the SEND Softkey to transmit the message Text Message Boxes Received text messages reside in the Inbox as Read or Unread messages The Outbox contains Sent and Unsent text messages Saved messages that are meant to be sent later are stored as Drafts Each text mes
156. splay the active flight plan Press the FMS Knob to activate the cursor v pu i8 ec Or for a stored flight plan a Press the FPL Key on the MFD b Turn the small FMS Knob to select the Flight Plan Catalog Page c Press the FMS Knob to activate the cursor d Turn the large FMS Knob to highlight the desired flight plan e Press the EDIT Softkey 2 Tum 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 saunyea4 aoueplony saunpa20Jd paezey jeuonippy uoneiedo Jeuuouqy 3 Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected procedure E or airway STORE A FLIGHT PLAN 1 After creating a flight plan on either the PFD or MED 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 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX x pul 45 Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index A Flight Planning GARMIN EDIT A STORED FLIGHT PLAN 1 2 3 4 5 6 1 Press the FPL Key on the MFD then
157. t Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 4 For a b o d Or Fo a b d Or A GARMIN Direct to planning Press the WPTS Softkey and verify that the starting waypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint point to point planning Enter the identifier of the starting waypoint Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again enter the identifier of the ending waypoint Press the ENT Key to accept the waypoint For flight plan leg planning a b o d Press 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 displays the active flight plan If an active flight plan is selected REM is an available option to dis
158. t plan only user waypoints These waypoints have been saved to the system user waypoints No flight plans stored in the system have been modified No flight plan files found to import The SD card contains no flight plan data Flight plan import failed Flight plan data was not successfully imported from the SD card Flight plan partially imported Some flight plan waypoints were success imported from the SD card however others had e stored flight plan novv exists in the system 4 ully rors and were not imported A partial File contained user waypoints only Th ab Su e file stored on the SD card did not contain flight plan only user waypoints One o more of these waypoints did not import ccessfully Too many points Flight plan truncated Th Th e flight plan on the SD card contains more waypoints than the system can support e flight plan was imported with as many waypoints as possible Some waypoints not loaded Waypoints locked m e flight plan on the SD card contains one ore waypoints that the system cannot in the navigation database The flight has been imported but must be edited ru in the system before it can be activated Se 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GK s m p q aoueplony SoJnpa204d buluueld AEN 540 S24V olpny uqax 7
159. tact Garmin Flight Data Services at 1 866 739 5687 in the United States or 913 397 8200 ext 1135 for assistance The GFDS weather data request area exceeds size limits Reduce weather coverage area and re send data request Request Cancelled Requested area too large Reduce coverage area The user has cancelled a GFDS weather data request The size of the GFDS weather data request has exceeded limits Reduce the size of the coverage area and try the weather data request again Request Failed Try Again Transfer Preempted The weather data request timed out Re send data request The datalink is busy Retry request later Cancelling a GFDS Weather Data Request in Progress 1 2 3 4 Select the GFDS Weather Data Link Page Press the MENU Key With GFDS Data Request highlighted press the ENT Key Turn the large FMS Knob to select CANCEL REQ and press the ENT Key The request status box indicates Request Cancelled 5 Press the FMS Knob to return to the GFDS Weather Datalink Page Enabling Automatic GFDS Data Requests 1 2 3 4 Select the GFDS Weather Data Link Page Press the MENU Key With GFDS Weather Request highlighted press the ENT Key Choose the desired weather coverage options 5 62 Turn the large FMS Knob to select the UPDATE RATE setting Then turn the small FMS Knob to highlight the desired automatic update frequency OFF 5 Min 10 Min
160. the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Terrain database mismatch The PFD and MFD have different terrain database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Obstacle database mismatch The PFD and MFD have different obstacle database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on NAV DB UPDATED Active navigation database updated System has updated the active navigation database from the standby navigation database TERRAIN DSP PFD1 or MFD1 Terrain awareness display unavailable One of the terrain or obstacle databases required for HTAWS in the specified PFD or MFD is missing or invalid GMA 350H MESSAGE ADVISORIES Message GMAT FAIL GMAT is inoperative Comments The audio panel self test has detected a failure The audio panel is unavailab
161. tion 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This does not delete the stored flight plan only the active flight plan VERTICAL NAVIGATION VNAV 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 ACTIVE FLIGHT PLAN 190 01254 00 Rev B C VTE LEMYN 11 7NH 9 QNM 8 0 Approach KDFH RNAV 17Leps RIVET inf DRAAK INWOD MENOL faf RW17L map 99 FT POLKE 18 8NH 3 3NH 2NM S Ul Oo CO CO 1 Wale 1 Large White 12400FT q B rrT 2000 Sma Sma 9900FT Large Light Blue Text m t Blue Subdued Text Il White Text ext Blue Text Light Erle with Altitude Res SIUE Cross AT or ABOVE 5 000 fi Fac Cross AT 2 300 ft ciao Cross AT or BELOW 3 000 ft Garmin G1000H Cockpit Reference Guide for the Bell 407GX riction Bar 33 svol4 sjueumajsul sub oipny uddx U10 AeN Suelv uoneiedo sainjea4 2 Duruue d Tunuuy Jeuuouqy Jeuonippy paezey nu xipuaddy x pul Flight Instrume
162. tion Page Press the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD DIS radial distance Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT
163. to display the Active Flight Plan Page Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan 4 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX sjuauimasu UTE 5721 oipny uddx UI0JNeN 52 2 4 AEN 540 nubi eouepioAy paezey suelv uoneiedo sainjea4 unuuy qeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning GARMI N 3 4 5 The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion point Press the LD WPT Softkey The selected waypoint is inserted at the selected point The default user waypoint naming is USR000 USR001 USR002 and 50 on To change the user waypoint name follow the procedure for modifying a user waypoint EXPORT A FLIGHT PLAN TO AN SD CARD 1 2 3 4 5 6 1 48 NOTE See the Annunciations amp Alerts section for flight plan export message descriptions Ins
164. transceiver is selected for transmitting by pressing the MIC Keys on the Audio Panel During reception of audio from the COM radio selected for transmission audio from the other COM radio is muted An active COM frequency displayed in green indicates that the COM transceiver is selected on the Audio Panel MICI or MIC2 Key Frequencies in the standby field are displayed in either white or gray The standby frequency in the tuning box is white The other standby frequency is gray 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX sjueuimasu sub 52 oipny uadx 5721 U10 AEN sualy uoneJado soJnjeoJ 2 AEN 5649 junuuy jeuuouqy Jeuonippy paezey nubi xipueddy x pul Nav Com AFCS XPDR Audio EICAS Abnormal Additional Hazard Annun Flight Instruments Flight Planning GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN Active Standby Fields Fields 135 100 Tuning Box COM2 Radio is Selected on the Audio Panel Selecting a COM Radio for Transmit SELECTING A NAV RADIO A NAV radio is selected for navigation by pressing the CDI Softkey located on the PFD The active NAV frequency selected for navigation is displayed in green Pressing the CDI Softkey once selects NAVI as the navigation radio Pressing the CDI Softkey a second time selects NAV2 as the navigation
165. ts EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 6 1 8 9 A GARMIN The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select LAT LON latitude and longitude Press the ENT Key CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 38 1 2 3 4 5 6 7 8 9 10 Turn the large FMS Knob on the MFD to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Press the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the 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
166. um Transmission in the menu list Press the ENT Key The Iridium transceiver is now disabled To enable the Iridium transceiver repeat steps 1 through 4 then select Enable Iridium Transceiver Telephone Communication The pilot or copilot can place and answer calls on the Iridium satellite network Control and monitoring of telephone functions are accomplished through the AUX TELEPHONE Page To view the Telephone Page 1 2 78 Turn the large FMS Knob on the MFD to select the AUX page group Turn the small FMS Knob to select the AUX TELEPHONE Page Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Additional Features nternal Phone External Phone Description Phone is Idle e n e is ringing n e has a dial tone off hook or connected to another e n e dialed is busy n e is dialing another phone n e has failed o n e status not known 0 n e is disabled Phone is reserved for data transmission Calling other phone or incoming call from other phone Other phone is on hold Phones are connected 190 01254 00 Rev B 19 Garmin G1000H Cockpit Reference Guide for the Bell 407GX xipueddy suelv uoneiedo sainjea4 aoueplony SoJnpa20Jd buluueld AEN Sd5 S24
167. uouqy Jeuonippy x pul GARMIN itional Features Add Blank Page 6 2 4 x pul 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 4076X 96 GARMI N LL Abnormal Operation ABNORMAL OPERATION REVERSIONARY MODE Should a system detected failure occur in either display the G1000H automatically enters reversionary mode In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display Reversionary display mode can be manually activated by pressing the DU BACKUP Button on the instrument panel NOTE The Bell 407GX Rotorcraft Flight Manual RFM always takes precedence over the information found in this section ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected In the event of a failure of both PFDs the emergency frequency 121 500 MHz automatically becomes the active frequency on both COM radios HAZARD DISPLAYS WITH LOSS OF GPS POSITION If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are removed until GPS position is again established Loss of Hazard Functions with Loss of GPS Position 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX 97 uep ony Senp
168. urce is coming from a unique location or seat position Because this feature uses different signals for left and right channels it requires wiring for stereo intercom and stereo headsets If 3D audio is activated when mono headsets are in use the listener will still hear all audio sources however there is no benefit from location separation With a single COM selected and 3D Audio enabled the listener hears the audio source at the 12 o clock position If all three COMs are selected the listener hears the audio sources at the 11 12 and 1 o clock positions with the COM numbers increasing clockwise If two COMs are selected the listener hears COMI at the 11 o clock position and COM2 at the 1 o clock position All other intercom positions are processed to sound like their relative seat location By default the GMA 350H assumes the pilot sits in the right seat A Garmin authorized service center can make changes to the default configuration ENABLING 3D AUDIO Press and hold the PILOT Key to toggle 3D audio processing on and off for all headset positions When 3D Audio is enabled the aural message 3D audio left is heard in the left ear followed by 3D audio right in the right ear 3D AUDIO TROUBLESHOOTING Ifthe aural messages are not heard in only the left and then the right ear respectively the cause may be aircraft wiring or headset settings Refer to the following table if a headset or aircraft wiring problem is suspected 20 Ga
169. ure to 29 92 in Hg a 1013 hPa 2 optional xs SE one a ov RA STS 5 5 73 4 75 us r NN KS EY buluueld Wil TC T r Tar Josse ee ee 5 umu m r r m rs Press the BACK Softkey to return to the top level softkeys s snp old paezey 3333 Ts TT Tem ss T sex qp sse a 7 73 7 7 7 7 7 74 Press the BACK Softkey to return to the previous level softkeys saunjeaj jeuonippy Transponder Softkeys uoneiedo Jeuuouqy Level 1 Level 2 Level 3 Description XPDR Displays transponder mode selection 5 softkeys 88 STBY Selects Standby Mode transponder does not reply to any interrogations 3 ON Selects Mode A transponder replies to z interrogations zi g x 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS KPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix A GARMIN Level 1 Level 2 Level 3 Description IDENT TMR REF NRST MSG ALT GND VFR CODE IDENT 0 7 BKSP Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely
170. ursor Turn either FMS Knob to select the desired message Press the MRK READ Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Mark Selected Message As Read Press the ENT Key The message symbol now indicates the message has been opened Mark AlI Messages As Read 1 2 3 4 While viewing the Inbox on the AUX TEXT MESSAGING Page press the MENU Key to display the Page Menu Turn either FMS Knob to place the cursor on Mark All New Messages As Read Press the ENT Key A confirmation window is displayed With cursor highlighting YES press the ENT Key The message symbols now indicate all the message have been opened Delete a Message 1 2 3 While viewing the Inbox on the AUX TEXT MESSAGING Page press the FMS Knob to activate the cursor Turn either FMS Knob to select the desired message Press the DELETE Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Delete Selected Message Press the ENT Key Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Additional Features WI FI CONNECTIONS OPTIONAL Control and monitoring of Wi Fi functions are accomplished through the AUX WI FI SETUP Page Viewing the Wi Fi Setup Page 1 Tum the large FMS Knob on the MFD to select the AUX page group 2 Turn the small FMS
171. us Page press the FMS Knob to activate the cursor Turn the large FMS Knob to move the cursor to the send button on the desired data report Press the ENT Key Restore Reports Page Options to Default Settings While viewing the Report Status Page press the MENU Key Turn the FMS Knob to select Restore Defaults in the menu list Press the ENT Key A confirmation window is now displayed Turn the large FMS Knob to select YES or NO With YES highlighted press the ENT Key SIRIUSXM RADIO ENTERTAINMENT OPTIONAL 92 The XM Radio Page provides information and control of the audio entertainment features of the SiriusXM 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 Press the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B GARMIN Ad itional 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 Press the CATGRY Softkey on the XM Radio Page 2 Pr
172. 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 118 Garmin G1000H Cockpit Reference Guide for the Bell 407GX 190 01254 00 Rev B A GARMIN Annunciations 8 Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message SLCT FREQ Select appropriate frequency for approach Comments The system notifies the pi lot to load the approach frequency for the appropriate NAV receiver Select the correct frequen Cy for the approach SLCT NAV Select NAV approach on CDI for The system notifies the pi correct NAV receiver Set NAV receiver lot to set the CDI to the the CDI to the correct PTK FAIL Parallel track unavailable Bad AA ctt bad geometry P ib y IAF waypoint for parallel offset has been passed past IAF 5 IAF waypoint for parallel offset has been passed UNABLE V WPT Can t vertical waypoint each current The current vertical waypoi ight path angle and vertical within the maximum f nt can not be reached speed constraints The system automatically transitions to the next vertical waypoint VNV Unavailable Excessive track angle error The current track angle e causing the vertical devia or exceeds the limit tion to go invalid VNV Unavailable
173. valid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000H uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircrafts current estimated position NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000H stops navigating in GPS Mode DR Mode is indicated on the G1000H by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure Also the CDI deviation bar is removed from the display Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS SBAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000H in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of estimating your positio
174. ved from the navigation database and is provided as a reference Garmin G1000H Cockpit Reference Guide for the Bell 407GX White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the Altitude has been entered The system cannot system estimating the by the pilot Altitude is use this altitude in altitude of the aircraft as it designated for use in determining vertical passes over the navigation giving vertical flight path 1 flight path guidance point This altitude is guidance Altitude does provided as a reference not match the published and is not designated to altitude in navigation be used in determining database or no published vertical flight path altitude exists guidance Small Text Altitude is not designated 1 Altitude is designated for The system cannot use in giving vertical flight path guidance Altitude has been retrieved 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 190 01254 00 Rev B A GARMIN WEIGHT PLANNING Flight Planning FLIGHT PLANNING All procedures apply to the MFD unless otherwise stated Entering Payload Parameters Turn the large FMS Knob to select the AUX page group Tum the small FMS Knob to select the Weight Planning Page 1 Press the EMPTY VT Softkey to place the cursor in the Ba
175. with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan longer exists in any database Or update the waypoint name identifier to refle the new information if it no t CY FPL WPT MOVE Flight plan waypoint moved The system has detected that a waypoint coordinate has changed due to a new navigation databas update Verify that stored flight plans contain correct waypoint locations D TIMER EXPIRD Timer has expired The system notifies the pilot that the timer has expired 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX saunjeaj aoueplony s mp oold Buruue d AEN Sd5 yi oipny uddx sv l3 siu u nnsu paezey u102 AEN nubi euonippv uoneiedo Jeuuouqy EY x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations 8 Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message DB CHANGE Database changed Verify user modified procedures Comments This occurs when procedures that have been manually edited This ly after an navigation database f alert is issued on update Verify th in stored flight p a stored flight p at the user modi ans are correct a an contains ied procedures nd up to date DB CHANGE Database changed V
176. yed With YES highlighted press the ENT Key 190 01254 00 Rev B Garmin G1000H Cockpit Reference Guide for the Bell 407GX s tin sul Yid 5721 oipny uddx JUI0JNeN 52 2 4 AEN 540 nubi aoueplony paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A FLIGHT PLAN 42 NOTE When creating a flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Creating an active flight plan 1 2 3 4 5 6 Press the FPL Key Press the FMS knob to activate the cursor only on MFD Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key The active flight plan is modified as each waypoint is entered Repeat step numbers 3 and 4 to enter each addition

Garmin 407GX Cockpit Reference Guide

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