Manual Garmin G1000H

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  • Garmin G1000H - page 1

    G1000H ™ Integrated Flight Deck Pilot’ s Guide Bell 407GX ...

  • Garmin G1000H - page 2

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  • Garmin G1000H - page 3

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX Copyright © 2011 Garmin Ltd. or its subsidiaries . All rights reserved. T his manual reflects the operation of System Softw are version 1237.03 or later for the Bell 407GX Helicopter . Some differences in operation may be observed when comparing the information in this man ...

  • Garmin G1000H - page 4

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B ii LIMITED W ARRANTY LIMITED W ARRANTY Within the warr anty period, Garmin will, at its sole discretion, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts and/or labor incidental to the d ...

  • Garmin G1000H - page 5

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX iii W ARNINGS , CAUTIONS , AND NOTES WARNING: Navigation and terrain separation must NO T be predicated upon the use of the terrain avoidance feature . T he terrain avoidance feature is NO T intended to be used as a primary reference for terrain avoidance and does not reliev ...

  • Garmin G1000H - page 6

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B iv W ARNINGS , CAUTIONS , AND NOTES WARNING: The United States government operates the Global P ositioning System and is solely responsible for its accuracy and maintenance . T he GPS system is subject to changes which could affect the accuracy and performance of all GPS equ ...

  • Garmin G1000H - page 7

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX v W ARNINGS , CAUTIONS , AND NOTES NOTE: All visual depictions contained within this document, including screen images of the panel and displays , are subject to change and may not reflect the most current system and databases . Depictions of equipment may differ slightly f ...

  • Garmin G1000H - page 8

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B vi REVISION INFORMA TION Record of Revisions P art Number Revision Date P age Range Description 190-01255-00 A B F ebruary , 2011 September , 2011 All All Initial release Added 3D Audio and Voice Recognition V arious clerical changes ...

  • Garmin G1000H - page 9

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX vii T ABLE OF CONTENTS SECTION 1 SYSTEM O VERVIEW 1.1 System Description ................................................. 1 1.2 Line Replaceable Units (LRU) ................................. 2 1.3 G1000H Controls ..................................................... 6 PFD C ...

  • Garmin G1000H - page 10

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B viii T ABLE OF CONTENTS Mono/Stereo Headsets .............................................. 123 Intercom .................................................................. 123 Clearance Recorder and Player (Optional) ................... 129 Split COM ........................ ...

  • Garmin G1000H - page 11

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX ix T ABLE OF CONTENTS SECTION 7 AUT OMA TIC FLIGHT CONTROL SYSTEM SECTION 8 ADDITIONAL FEA TURES 8.1 Synthetic Vision System (SVS) ........................... 376 SVS Operation .......................................................... 377 SVS F eatures ..................... ...

  • Garmin G1000H - page 12

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B x T ABLE OF CONTENTS B lank P age ...

  • Garmin G1000H - page 13

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 1 SY STEM OVER VIEW SECTION 1 SY STEM OVER VIEW 1.1 SY STEM DESCRIPTION This section provides an overview of the G1000H Integrated Flight Deck as installed in the Bell 407GX. The G1000H system is an integrated flight control system that pr esents flight instrumentation, po ...

  • Garmin G1000H - page 14

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 2 SY STEM OVER VIEW 1.2 LINE REPLA CEABLE UNITS (LRU) • GDU 1040H (2) – One unit is configured as a PFD, the other as an MFD, each featuring a 10.4-inch LCD with 1024 x 768 resolution. The unit installed on the right/pilot side is designated as the PFD, and the one i ...

  • Garmin G1000H - page 15

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 3 SY STEM OVER VIEW • GSC 46 (1) – The GSC 46 is a signal conditioner which converts tachometer and engine torque information to a digital format for use by the GEA 71H. • GRS 77H (1) – Provides air craft attitude and heading information via ARINC 429 to both G ...

  • Garmin G1000H - page 16

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 4 SY STEM OVER VIEW • GDL 69AH (1) – A satellite radio receiver that pr ovides real-time weather information to the G1000H MFD (and, indirectly , to the inset map of the PFD) as well as digital audio entertainment. The GDL 69AH communicates with the MFD via HSDB conne ...

  • Garmin G1000H - page 17

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 5 SY STEM OVER VIEW • GA 58 (2) – The GA 58 are directional antennas for the T raffic A voidance System. One top-mounted directional antenna is required. Optional bottom mounted antenna of fers better threat visibility . • GA 36 (1) and GA 37 (1) – The GA 36 i ...

  • Garmin G1000H - page 18

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 6 SY STEM OVER VIEW 1.3 G1000H CONTROLS NOTE: T he Audio P anel (GMA 350) are described in the CNS & Audio P anel. The G1000H system controls ar e located on the PFD and MFD bezels and audio panel. The controls for the PFD and MFD are discussed within the following pages ...

  • Garmin G1000H - page 19

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 7 SY STEM OVER VIEW 5 Joystick T urn to change map range Press to activate Map Pointer for map panning 6 CRS/BARO Knob T urn large knob for altimeter bar ometric pressure setting T urn small knob to adjust course (only when HSI is in VOR or OBS Mode) Press to re-center the C ...

  • Garmin G1000H - page 20

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 8 SY STEM OVER VIEW The N AV , CRS/BARO , COM , FMS , and A LT knobs are concentric dual knobs, each having small (inner) and large (outer) contr ol portion. When a portion of the knob is not specified in the text, either may be used. Large (Outer) Knob Small (Inner) Knob F ...

  • Garmin G1000H - page 21

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 9 SY STEM OVER VIEW 8 MUSIC Key Selects and deselects music audio. 9 MAN SQ Key Manual Squelch annunciator . When lit, squelch is controlled manually . 10 V olume Indicator Indicates volume/squelch setting relative to full scale. 11 Front Panel Jack Used for an entertainment ...

  • Garmin G1000H - page 22

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 10 SY STEM OVER VIEW 1.4 SECURE DIGIT AL CARDS NO TE: Refer to the Appendices for instructions on updating the aviation database . NO TE: Ensure that the G1000H system is powered off before inserting the SD card. The PFD and MFD data car d slots use Secure Digital (SD) cards ...

  • Garmin G1000H - page 23

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 11 SY STEM OVER VIEW 1.5 SY STEM POWER-UP NOTE: Refer to the Appendices for AHRS initialization bank angle limitations . NOTE: See the Appendices for additional information regarding system-specific annunciations and alerts . NOTE: See the Rotorcraft Flight Manual Supplemen ...

  • Garmin G1000H - page 24

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 12 SY STEM OVER VIEW 1.6 SY STEM OPERA TION NO TE: In normal operating mode , backlighting can only be adjusted from the PFD . In reversionary mode , it can be adjusted from the remaining display . The displays are connected together via a single Ethernet bus for high-speed ...

  • Garmin G1000H - page 25

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 13 SY STEM OVER VIEW REVERSIONAR Y DISPLA Y OPERA TION NOTE: T he G1000H System alerts the pilot when backup paths are utilized by the LRUs . Refer to Appendix A for further information regarding system-specific alerts . In the event of a display failure, the G1000H System ...

  • Garmin G1000H - page 26

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 14 SY STEM OVER VIEW AHRS OPERA TION NOTE: Refer to the Appendices for specific AHRS alert information. NOTE: Aggressive maneuvering while the AHRS is not operating normally can degrade AHRS accuracy . In addition to using internal sensors, the GRS 77H AHRS uses GPS informa ...

  • Garmin G1000H - page 27

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 15 SY STEM OVER VIEW AIR D A T A INPUT F AILURE A failure of the air data input has no ef fect on AHRS output while AHRS is operating in normal mode. A failure of the air data input while the AHRS is operating in reversionary No-GPS mode results in invalid attitude and headi ...

  • Garmin G1000H - page 28

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 16 SY STEM OVER VIEW SOFTKEY FUNCTION The softkeys are located along the bottoms of the displays. The softkeys shown depend on the softkey level or page being displayed. The bezel keys below the softkeys can be used to select the appropriate softkey . When a softkey is selec ...

  • Garmin G1000H - page 29

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 17 SY STEM OVER VIEW Level 1 Level 2 Level 3 Description PFD Displays second-level softkeys for additional PFD configurations SYN VIS Displays the softkeys for enabling or disabling Synthetic V ision features P A THW A Y Displays rectangular boxes repr esenting the horizont ...

  • Garmin G1000H - page 30

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 18 SY STEM OVER VIEW Level 1 Level 2 Level 3 Description CDI Cycles through GPS, VOR1, and VOR2 navigation modes on the CDI DME Displays the DME T uning W indow , allowing selection of the DME XPDR Displays transponder mode selection softkeys STBY Selects standby mode (trans ...

  • Garmin G1000H - page 31

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 19 SY STEM OVER VIEW Figure 1-15 PFD Configuration Softk eys Press the BACK Softkey to return to the top-level softkeys AL T UNIT METERS IN HP A HSI FRMT 360 HSI ARC HSI (optional) SYN VI S SYN TERR HRZN HDG PAT HW AY APTSIGNS MSG MSG MSG MSG MSG MSG SET HD G CAS HDG -H PM ...

  • Garmin G1000H - page 32

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 20 SY STEM OVER VIEW MFD SOFTKEY S Level 1 Level 2 Level 3 Description ENGINE Displays the EIS-Engine Page CAS ↑ Scroll up (Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling) CAS ↓ Scroll down (Displa ...

  • Garmin G1000H - page 33

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 21 SY STEM OVER VIEW Level 1 Level 2 Level 3 Description DCL TR Selects desired amount of map detail; cycles through declutter levels: DCL TR (No Declutter): All map features visible DCL TR-1: Declutters land data DCL TR-2: Declutters land and SUA data DCL TR-3: Removes ever ...

  • Garmin G1000H - page 34

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 22 SY STEM OVER VIEW Viewing GPS r eceiver status information 1) Use the large FMS Knob on the MFD to select the Auxiliary P age Group (see Section 1.7 for information on navigating MFD page groups). 2) Use the small FMS Knob to select GPS Status P age . Selecting the GPS re ...

  • Garmin G1000H - page 35

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 23 SY STEM OVER VIEW The GPS Status Page provides the following information: • Satelliteconstellationdiagram Satellites currently in view are shown at their r espective positions on a sky view diagram. The sky view is always in a north-up orientation, with the out ...

  • Garmin G1000H - page 36

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 24 SY STEM OVER VIEW Because of the tighter protection limit on appr oaches, there may be times when RAIM is not available. The G1000H automatically monitors RAIM and warns with an alert message when it is not available. If RAIM is not predicted to be available for the fina ...

  • Garmin G1000H - page 37

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 25 SY STEM OVER VIEW Disabling WAAS , EGNOS or MSAS 1) Select the GPS Status P age . 2) If necessary , select the SBAS Softk ey . 3) Press the FMS Knob , and turn the large FMS Knob to hightlight the desired SBAS system. 4) Press the ENT K ey to uncheck the box. 5) Press the ...

  • Garmin G1000H - page 38

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 26 SY STEM OVER VIEW 1.7 A CCESSING G1000H FUNCTIONALITY MENUS The G1000H has a MENU Key that, when pressed, displays a context-sensitive list of options. This options list allows the user to access additional features or make settings changes which specifically relate to t ...

  • Garmin G1000H - page 39

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 27 SY STEM OVER VIEW MFD P A GE GROUPS NOTE: Refer to the Flight Management, Hazard Avoidance , and Additional F eatures sections for details on specific pages . Information on the MFD is presented on pages which ar e grouped accor ding to function. The page group and activ ...

  • Garmin G1000H - page 40

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 28 SY STEM OVER VIEW Figure 1-21 Map P ages Map Pages (MAP) Navigation Map T raffic Map W eather Data Link ( service optional ) HT A WS Figure 1-22 W aypoint P ages Airport Information Pages W aypoint Pages (WPT) Airport Information pages - Airport Information ( INFO-1 Soft ...

  • Garmin G1000H - page 41

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 29 SY STEM OVER VIEW Auxiliary Pages (AUX) W eights, Fuel, Exceedances T rip Planning Utility GPS Status System Setup - System Setup 1 ( SETUP 1 Softkey) - System Setup 2 ( SETUP 2 Softkey) XM Radio - XM Information ( INFO Softkey) - XM Radio ( RADIO Softkey) Satellite Phone ...

  • Garmin G1000H - page 42

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 30 SY STEM OVER VIEW The Flight Plan Pages may also be accessed using the FPL Key . Main pages within this group are selected by turning the small FMS Knob. The Checklist Page may be accessed from the page gr oup tab or the CHKLIST Softkey . See the Additional Features secti ...

  • Garmin G1000H - page 43

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 31 SY STEM OVER VIEW MFD SY STEM P A GES In the Auxiliary (AUX) Page Group, there ar e two system pages: System Setup and System Status. The System Setup Page allows management of various system parameters, while the System Status Page displays the status of all G1000H syste ...

  • Garmin G1000H - page 44

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 32 SY STEM OVER VIEW Figure 1-28 System Setup 2 P age D a te /t ime The Date/T ime Box on the System Setup 1 Page displays the current date and time and allows the pilot to set the time format (local 12-hr , local 24-hr , or UTC) and offset. The time of fset is used to defi ...

  • Garmin G1000H - page 45

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 33 SY STEM OVER VIEW D isPla y U nits Units in which various quantities are displayed on the G1000H scr eens are listed on the System Setup 1 Page. The Navigation Angle reference and the Position units ar e pilot selectable. Category Settings Affected Quantities Exceptions N ...

  • Garmin G1000H - page 46

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 34 SY STEM OVER VIEW B aRO t RansitiOn a leRt See the Flight Instruments section for a discussion on setting the Baro T ransition Alert. a iRsP ace a leR ts The Airspace Alerts Box allows the pilot to turn the controlled/special-use airspace message alerts on or off. This do ...

  • Garmin G1000H - page 47

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 35 SY STEM OVER VIEW 5) T urn the large FM S Knob to select the ON/OFF field in the Arrival Alert Box. 6) T urn the small FMS Knob clockwise to turn the airspace alert ON or counterclockwise to turn the alert OFF . 7) Press the FMS Knob to deactivate the cursor . Changing t ...

  • Garmin G1000H - page 48

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 36 SY STEM OVER VIEW The following data may be selected for display in each of the four fields of the Navigation Status Box. • Bearing(BRG) • Distance(DIS) • DesiredT rack(DTK) • EnRouteSafeAltitude(ESA) • EstimatedT ime? ...

  • Garmin G1000H - page 49

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 37 SY STEM OVER VIEW T o change COM channel spacing: 1) While on the System Setup 1 Page , press the FMS Knob momentarily to activate the flashing cursor . 2) T urn the large FMS Knob to highlight the channel spacing field in the COM Configuration Box. 3) T urn the small ...

  • Garmin G1000H - page 50

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 38 SY STEM OVER VIEW Figure 1-29 Pilot Profiles (System Setup P age) Creating a profile: 1) T urn the large FMS Knob to select the A UX Page group . 2) T urn the small FMS Knob to select System Setup . 3) Press the FMS Knob momentarily to activate the flashing cursor . 4) ...

  • Garmin G1000H - page 51

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 39 SY STEM OVER VIEW Renaming a profile: 1) While on the System Setup 1 or Setup 2 Page , press the FMS Knob momentarily to activate the flashing cursor . 2) T urn the large FMS Knob to highlight ‘RENAME’ in the Pilot Profile Box. 3) Press the ENT Ke y. 4) In the ‘R ...

  • Garmin G1000H - page 52

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 40 SY STEM OVER VIEW Enabling HT A WS voice callouts: 1) T urn the large FMS Knob to select the A UX Page group . 2) T urn the small FMS Knob to select System Setup . 3) If necessary , press the SETUP 2 Softk ey to select the System Setup 2 P age . 4) Press the FMS Knob mome ...

  • Garmin G1000H - page 53

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 41 SY STEM OVER VIEW UTILITY P AGE For flight planning purposes, timers, trip statistics, and a scheduler feature are pr ovided on the AUX - Utility Page. The timers available include a stopwatch-like generic timer , a total time in flight timer , and a record of the time ...

  • Garmin G1000H - page 54

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 42 SY STEM OVER VIEW 6) T o stop the timer , press the ENT K ey with ‘ST OP?’ highlighted. T he field changes to ‘RESET?’. 7) T o reset the timer , press the ENT K ey with ‘RESET?’ highlighted. T he field changes back to ‘ST AR T?’ and the digits are reset. ...

  • Garmin G1000H - page 55

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 43 SY STEM OVER VIEW t RiP s t a tistics The odometer and trip odometer recor d the total mileage traveled from the last r eset; these odometers can be reset independently . Resetting the trip odometer also resets the average trip gr oundspeed. Maximum groundspeed for the pe ...

  • Garmin G1000H - page 56

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 44 SY STEM OVER VIEW 1.8 DISPLA Y BA CKLIGHTING The G1000H display and control backlighting can be adjusted either automatically or manually . A UT OMA TIC ADJUSTMENT The existing instrument panel dimmer bus normally contr ols the PFD and MFD backlighting as well as the PFD ...

  • Garmin G1000H - page 57

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 45 SY STEM OVER VIEW Adjust key backlighting manually: 1) Press the MENU K ey on the PFD to display the PFD Setup Menu Window . ‘ A UT O’ becomes highlighted to the right of ‘PFD DSPL ’. Figure 1-33 Manual K ey Lighting Adjustment 2) T urn the large FMS Knob to highl ...

  • Garmin G1000H - page 58

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 46 SY STEM OVER VIEW B lank P age ...

  • Garmin G1000H - page 59

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 47 FLIGHT INSTRUMENTS SECTION 2 FLIGHT INSTRUMENTS WARNING: In the event that the airspeed, altitude , or heading indications become unusable , refer to the backup instruments . Increased situational awareness is provided by r eplacing the traditional instrument on the panel ...

  • Garmin G1000H - page 60

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 48 FLIGHT INSTRUMENTS 9 17 14 13 12 1 18 20 21 10 6 2 3 4 16 11 15 19 22 8 1 NA V Frequency Box 2 Airspeed Indicator 3 Current Heading 4 Groundspeed 5 Power Situation Indicator (PSI) 6 Selected Heading Bug 7 Dual T achometer 8 Outside Air T emperature (OA T) 9 Softkeys 10 Syst ...

  • Garmin G1000H - page 61

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 49 FLIGHT INSTRUMENTS 6 8 7 2 4 3 1 5 9 10 1 T raffic Annunciation 2 Radar Altimeter 3 Selected Heading 4 Wind Data 5 DME Information Window 6 Bearing Information Windows 7 Barometric Minimum Descent Altitude 8 Flight Plan Window 9 Annunciation Window 10 Selected Course 11 ...

  • Garmin G1000H - page 62

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 50 FLIGHT INSTRUMENTS 2.1 FLIGHT INSTRUMENTS AIRSPEED INDICA T OR NOTE: Refer to the Rotorcraft Flight Manual (RFM) for speed criteria. The Airspeed Indicator displays airspeed on a moving tape rolling number gauge.  The gr oundspeed is d ...

  • Garmin G1000H - page 63

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 51 FLIGHT INSTRUMENTS A TTITUDE INDICA T OR Attitude information isdisplayed over a virtual blue sky andbrown gr ound with a white horizon line. The AttitudeIndicatordisplaysthe pitch,roll,andsl ...

  • Garmin G1000H - page 64

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 52 FLIGHT INSTRUMENTS AL TIMETER The Altimeter displays 600 feet of barometric altitude values at a time on a moving tape rolling number gauge.  Numericlabels andmajor tickmarksar eshownat inte ...

  • Garmin G1000H - page 65

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 53 FLIGHT INSTRUMENTS The barometric pressure setting is displayed below the Altimeter in inches of mercury (in Hg) or hectopascals (hPa)when metricunitsar eselected. Adjustingthe altimeterbar omet ...

  • Garmin G1000H - page 66

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 54 FLIGHT INSTRUMENTS ABaroT ransitionAlertisprovidedtoalertthepilottochangethebarometricpr essuresettingwhencrossing the transition altitude in either direction. This is displayed by the flashing light blue bar ometric pr ...

  • Garmin G1000H - page 67

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 55 FLIGHT INSTRUMENTS VERTICAL DEVIA TION NOTE: The Glidepath Indicator is only shown for aircraft with GIA 63W Integrated Avionics Units when SB AS is available . The V ertical Deviation Indicator (VDI)is amagenta chevron indicatingthe baro- ...

  • Garmin G1000H - page 68

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 56 FLIGHT INSTRUMENTS HORIZONT AL SITU A TION INDICA T OR (HSI) The Horizontal Situation Indicator (HSI) displays a rotating compass card in a heading-up orientation.  Letters indicate the cardinal points and numeric? ...

  • Garmin G1000H - page 69

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 57 FLIGHT INSTRUMENTS The Arc HSI is a 140˚ expanded section of the compass r ose.  The Arc HSI contains a Course Pointer , combined T o/From Indicatorand asliding deviation indicator ,and? ...

  • Garmin G1000H - page 70

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 58 FLIGHT INSTRUMENTS Navigation angles (track, heading, course, bearing) are set on the AUX - System Setup Page and are either corrected tothe computed magnetic variation (‘Mag V ar’), reference ...

  • Garmin G1000H - page 71

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 59 FLIGHT INSTRUMENTS TURN RA TE INDICA T OR The T urn Rate Indicator is located directly above the rotating compass card.  T ick marks to the left and right of thelubber linedenote half-standard and? ...

  • Garmin G1000H - page 72

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 60 FLIGHT INSTRUMENTS When a bearing pointer is displayed, its associated information window is also displayed.  The Bearing Information windows (Figure 2-22) are displayed to the lower sides of t ...

  • Garmin G1000H - page 73

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 61 FLIGHT INSTRUMENTS HEADING PRESET MODE HeadingPresetModeallowsAHRSto computeheadingdatawithoutusingthemagneticsensingdevice.If a magnet anomaly occurs (either due to interference or magnetometer ...

  • Garmin G1000H - page 74

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 62 FLIGHT INSTRUMENTS COURSE DEVIA TION INDICA T OR (CDI) N OT E : During a heading change of greater than 105˚ with respect to the course , the CDI on the Arc HSI switches to the opposite side of the deviation scale and displays reverse sensing. The Course Deviation Indicato ...

  • Garmin G1000H - page 75

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 63 FLIGHT INSTRUMENTS Changing navigation sources: 1) Select the CDI Softk ey to change from GPS to VOR1 or LOC1. T his places the light blue tuning box over the NA V1 standby frequency in the upper left corner of the PFD . 2) Select the CDI Softk ey again to change from VOR ...

  • Garmin G1000H - page 76

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 64 FLIGHT INSTRUMENTS GPS CDI SCALING When GPS is the selected navigation source, the ight plan legs ar e sequenced automatically and annunciations appear on the HSI for the ight phase.  Flight ...

  • Garmin G1000H - page 77

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 65 FLIGHT INSTRUMENTS Figure 2-29 Automatic CDI Scaling 2.0 nm Enroute (Oceanic if >200 nm from nearest airpor t) 0.3 nm Missed Approach 1.0 nm Approach 1.0 nm Te rminal 1.0 nm Te rminal 0.3 nm Depar ture CDI Full-scale Deflection Refer to accompan ying approach CDI scali ...

  • Garmin G1000H - page 78

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 66 FLIGHT INSTRUMENTS Figure 2-30 T ypical LNA V and LNA V+V Approach CDI Scaling 1.0 nm 2 nm 350 ft angle set by system 0.3 nm F AF CDI Full-scale Deflection CDI scale is set to the smaller of 0.3 nm or an angle set by the system CDI scale va ries if VTF is activated Figure 2 ...

  • Garmin G1000H - page 79

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 67 FLIGHT INSTRUMENTS OBS MODE NOTE: VNV is inhibited while automatic waypoint sequencing has been suspended. Enabling Omni-bearing Selector (OBS) Mode suspends the automatic sequencing of waypoints in a GPS ight plan (GPS? ...

  • Garmin G1000H - page 80

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 68 FLIGHT INSTRUMENTS As the aircraft cr osses the missed approach point (MAP), automatic appr oach waypoint sequencing is suspended.  ‘SUSP’ appears on the HSI at the lower right of the air c ...

  • Garmin G1000H - page 81

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 69 FLIGHT INSTRUMENTS 2.2 SUPPLEMENT AL FLIGHT DA T A NOTE: Selecting the DFL TS Softk ey turns off metric Altimeter display , the Inset Map , and wind data display . In addition to the flight instruments, the PFD also displays various supplemental information, including te ...

  • Garmin G1000H - page 82

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 70 FLIGHT INSTRUMENTS WIND D A T A W inddirectionandspeed(relativetotheair craft)inknotscanbedisplayedinawindowtotheupperleftof theHSI.Whenthewindowisselectedfordisplay ,butwindi ...

  • Garmin G1000H - page 83

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 71 FLIGHT INSTRUMENTS VERTICAL NA VIGA TION (VNV) INDICA TIONS When aVNV ight planhas been activated,VNV indications (VNVT arget Altitude, RSVI,VDI) appear onthe PFD in conjunction with the “TOD wit ...

  • Garmin G1000H - page 84

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 72 FLIGHT INSTRUMENTS 2.3 PFD ANNUNCIA TIONS AND ALERTING FUNCTIONS The following annunciations and alerting functions aredisplayed on the PFD.  Refer to the Engine Indication andCrewAlertingSystem(EICAS)Section ...

  • Garmin G1000H - page 85

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 73 FLIGHT INSTRUMENTS TRAFFIC ANNUNCIA TION T rafc is displayed symbolically on the PFD Inset Map, the MFD Navigation Map Page, and various other MFD page maps.  Refer to the Hazar d A voidance ...

  • Garmin G1000H - page 86

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 74 FLIGHT INSTRUMENTS AL TITUDE ALERTING The Altitude Alerting function provides visual and audio alerts when appr oaching the Selected Altitude.  Wheneverthe SelectedAltitude ischanged, AltitudeAlertingis ...

  • Garmin G1000H - page 87

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 75 FLIGHT INSTRUMENTS MINIMUM DESCENT AL TITUDE/DECISION HEIGHT ALERTING For altitude awar eness, a MinimumDescent Altitude (MDA) or DecisionHeight (DH), based on bar ometric altitude or radar altitude, can be set. ...

  • Garmin G1000H - page 88

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 76 FLIGHT INSTRUMENTS RAD AR AL TIMETER When the radar height (the aircraft altitude above ground level detected by the radar altimeter) is between zeroand2500feet,thecurrentvalueisdisplayedingree ...

  • Garmin G1000H - page 89

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 77 FLIGHT INSTRUMENTS A gr ound line (Figure2-49) is shownon the Altimeter todisplay the air craft’ s height relativeto the gr ound.  If the data becomes invalid,the message “RA F AIL”? ...

  • Garmin G1000H - page 90

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 78 FLIGHT INSTRUMENTS 2.4 ABNORMAL OPERA TIONS ABNORMAL GPS CONDITIONS TheannunciationslistedinT able2-3canappearonthe HSIwhenabnormalGPSconditionsoccur .Referto theFlightManagementSectionformoreinforma ...

  • Garmin G1000H - page 91

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 79 FLIGHT INSTRUMENTS UNUSU AL A TTITUDES When the aircraft enters an unusual pitch attitude, red chevrons pointing towar d the horizon warn of extreme pitch.  The chevrons are displayed on the Attitu ...

  • Garmin G1000H - page 92

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 80 FLIGHT INSTRUMENTS B lank P age ...

  • Garmin G1000H - page 93

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 81 ENGINE INDICA TION & CREW ALERTING SYSTEM SECTION 3 ENGINE AND CREW ALERTING SYSTEMS NOTE: Refer to the Rotorcraft Flight Manual (RFM) for limitations . The G1000H Integrated Flight Deck of fers improved flight operations and reduces pilot workload by automatically m ...

  • Garmin G1000H - page 94

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 82 ENGINE INDICA TION & CREW ALERTING SYSTEM In a display fails, the other display may be configured to present Primary Flight Display (PFD) symbology together with condensed EIS information (refer to the System Overview for more information about Reversionary Mode). EI ...

  • Garmin G1000H - page 95

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 83 ENGINE INDICA TION & CREW ALERTING SYSTEM 3.1 ENGINE INDICA TION SYSTEM (EIS) STRIP NOTE: Depictions of equipment may differ from the installed equipment. Examples shown may differ from the actual aircraft configuration. EIS information is presented using gauges and ...

  • Garmin G1000H - page 96

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 84 ENGINE INDICA TION & CREW ALERTING SYSTEM 9 7 8 10 5 3 4 2 1 Figure 3-3 MFD EIS Strip (Normal) 6 10 7 8 5 4 3 2 1 Figure 3-4 EIS Strip (Reversionary) 6 ...

  • Garmin G1000H - page 97

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 85 ENGINE INDICA TION & CREW ALERTING SYSTEM 3.2 ENGINE POWER AND SPEED INDICA TIONS NO TE : Refer to the Rotorcraft Flight Manual (RFM) for engine operating limitations and corrective actions . The Power Situation Indicator (PSI) and Dual T achometer are shown as a grou ...

  • Garmin G1000H - page 98

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 86 ENGINE INDICA TION & CREW ALERTING SYSTEM T AKEOFF TIMER After the engine has been started, if Q or MGT are within the takeof f limitation ranges, the G1000H displays a 5-minute countdown timer inside the PSI gauge. The timer flashes beginning when 30 seconds remain ...

  • Garmin G1000H - page 99

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 87 ENGINE INDICA TION & CREW ALERTING SYSTEM 3.3 ENGINE P AGE NO TE : Refer to the Rotorcraft Flight Manual (RFM) for engine operating limitations and corrective actions . Pressing the ENGINE Softkey on the MFD accesses the EIS - Engine Page, which displays all engine, e ...

  • Garmin G1000H - page 100

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 88 ENGINE INDICA TION & CREW ALERTING SYSTEM POWER ASSURANCE CHECK The G1000H can assist the pilot in performing a power assurance check to determine if installed specification power can be achieved. NOTE: F ollow the procedures in the Rotorcraft Flight Manual (RFM) for ...

  • Garmin G1000H - page 101

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 89 ENGINE INDICA TION & CREW ALERTING SYSTEM 3.4 CREW ALERTING SYSTEM (CAS) NOTE: Aural alerts associated with abnormal conditions and advisories are managed through the audio panels . Refer to the Audio P anel and CNS Section for more information. When Crew Alerting Sys ...

  • Garmin G1000H - page 102

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 90 ENGINE INDICA TION & CREW ALERTING SYSTEM MFD Alerts window containing CAS messages CAS Scrolling Softkeys (Disabled Until More Than 19 Messages are Displayed) Figure 3-10 Engine P age CAS Display (MFD) CAS MESSA GE PRIORITIZA TION NOTE: Information on CAS messages in ...

  • Garmin G1000H - page 103

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 91 ENGINE INDICA TION & CREW ALERTING SYSTEM NOTE: See the Rotorcraft Flight Manual (RFM) for recommended pilot actions . Annunciation T ext Description Audio Alert B A TTER Y HO T Battery overheat detected. Single Chime ENGINE FIRE Fire/Overheat detector senses a temper ...

  • Garmin G1000H - page 104

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 92 ENGINE INDICA TION & CREW ALERTING SYSTEM Annunciation T ext Description Audio Alert Q MISCOMP Q miscompare event. Single Ping R/FUEL BOOST Right fuel boost pump has failed. R/FUEL XFR Right fuel transfer pump has failed. T/R CHIP T/R Chip Detector has detected debris ...

  • Garmin G1000H - page 105

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 93 A UDIO P ANEL AND CNS SECTION 4 A UDIO P ANEL AND CNS 4.1 O VERVIEW The Communication/Navigation/Surveillance (CNS) system includes the Audio Panel, communication radios, navigation radios, and Mode S transponder . The System Over view Section pr ovides a block diagram de ...

  • Garmin G1000H - page 106

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 94 A UDIO P ANEL AND CNS MFD/PFD CONTROLS AND FREQUENCY DISPLA Y Figure 4-1 MFD/PFD Controls , NA V/COM Frequency T uning Boxes , and DME T uning Window 12 3 4 5 9 10 11 7 8 6 1 2 ...

  • Garmin G1000H - page 107

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 95 A UDIO P ANEL AND CNS 1 NA V VOL/ID Knob – Controls NA V audio volume level. Press to turn the Morse code identifier audio on and off. V olume level is shown in the NA V frequency field as a per centage. 2 NA V Frequency T ransfer Key – T ransfers the standby and ac ...

  • Garmin G1000H - page 108

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 96 A UDIO P ANEL AND CNS A UDIO P ANEL CONTROLS Figure 4-2 GMA 350H Audio P anel Controls 21 14 15 17 12 13 11 19 20 18 16 10 8 6 4 2 3 5 7 9 1 NOTE: When a k ey is selected, a triangular annunciator above the key is illuminated. 1 MKR/MUTE – Selects marker beacon receiver ...

  • Garmin G1000H - page 109

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 97 A UDIO P ANEL AND CNS 12 MIC1  – Selects the #1 transmitter for transmitting.  COM1 receive is simultaneously selected when this key is pressedallowing received audiofr omthe #1 COM receiver? ...

  • Garmin G1000H - page 110

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 98 A UDIO P ANEL AND CNS 4.2 COM OPERA TION COM TRANSCEIVER SELECTION AND ACTIV A TION NO TE: When turning on the system for use , the system remembers the last frequencies used and the active COM transceiver state prior to shutdown. The COM Frequency Box is comp ...

  • Garmin G1000H - page 111

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 99 A UDIO P ANEL AND CNS TRANSMIT/RECEIVE INDICA TIONS During COM transmission, a white TX appears by the active COM frequency r eplacing the Frequency T ransfer Arr ow . On the Audio Panel, when PTT is pressed, the active transce ...

  • Garmin G1000H - page 112

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 100 A UDIO P ANEL AND CNS SELECTING THE RADIO T O BE TUNED Press the small COM  Knob to transfer the frequency tuning box and Frequency T ransfer Arrow between the upper and lower radio frequency fields. Figure 4-6 Switching COM T u ...

  • Garmin G1000H - page 113

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 101 A UDIO P ANEL AND CNS A UT O-TUNING THE COM FREQUENCY COM frequencies can be automatically tuned fr om the following: • NearestAirportsW indow(PFD) • WPT–AirportInformationPage • NRST–NearestAirportsPage • NRST? ...

  • Garmin G1000H - page 114

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 102 A UDIO P ANEL AND CNS A UT O-TUNING FROM THE MFD Frequencies can be automatically loaded into the COM Frequency Box from pages in the NRST or WPT page group by highlighting the fr equency and pressing the ENT Key(F ...

  • Garmin G1000H - page 115

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 103 A UDIO P ANEL AND CNS On the WPT - Airport Information Page, the cursor can be placed on the fr equency eld by pressing the FMS  Knob and scrollingthrough the list.  The frequency i ...

  • Garmin G1000H - page 116

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 104 A UDIO P ANEL AND CNS COM frequencies can also be auto-tunedfr om the NRST–Nearest Airspaces, NRST–Nearest Frequencies, and NRST–Nearest Airports Pageson theMFD ina similarmanner ...

  • Garmin G1000H - page 117

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 105 A UDIO P ANEL AND CNS FREQUENCY SP A CING TheCOM radioscantuneeither 25-kHzspacing(118.000 to136.975MHz) or8.33-kHzspacing (118.000 to 136.990 MHz) for 760-channel or 3040-channel conguration.  ...

  • Garmin G1000H - page 118

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 106 A UDIO P ANEL AND CNS A UT OMA TIC SQUELCH Automatic COM Squelch quiets unwanted static noise when no audio signal is received, while still pr oviding good sensitivity to weak COM signals. T o disable Automatic COM Squelch, press the VOL/SQ Knob.  When Automatic ...

  • Garmin G1000H - page 119

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 107 A UDIO P ANEL AND CNS 4.3 NA V OPERA TION NA V RADIO SELECTION AND ACTIV A TION The NA V Frequency Box is composed of four elds; two standby fields and two active fields. The active frequencies are on the right side and the standby fr e ...

  • Garmin G1000H - page 120

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 108 A UDIO P ANEL AND CNS NA V radios are selected for listening by pr essing the corresponding keys on the Audio Panel. Pressing the NA V1 ,or NA V2 Key selects and deselects the navigation radio sour ce. Selected audio can be heard over the headset and the speaker (if sele ...

  • Garmin G1000H - page 121

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 109 A UDIO P ANEL AND CNS SELECTING THE RADIO T O BE TUNED Press the small N AV Knob totransfer thefrequency tuningbox andFrequency T ransferArr owbetween the upper and lower radio frequency fields. Figure 4-20 Switching NA V T unin ...

  • Garmin G1000H - page 122

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 110 A UDIO P ANEL AND CNS A UT O-TUNING A NA V FREQUENCY FROM THE MFD NA Vfrequenciescanbeselectedandloadedfr omthefollowingMFDpages: • WPT–AirportInformation • WPT–VORInformation • NRST–Nearest ...

  • Garmin G1000H - page 123

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 111 A UDIO P ANEL AND CNS Or : 1) When on the Nearest VOR, Nearest Airspaces, and Nearest Airports pages , press the MENU K ey to display the page menu. 2) T urn the large FMS Knob to scroll through the menu options . 3) Press the ENT K ey to place the cursor in the desired ...

  • Garmin G1000H - page 124

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 112 A UDIO P ANEL AND CNS In the example shown, theVOR list is selected with the VOR Softkey or from the page menu. The FMS Knob or ENT Key is used to scroll thr ough the list. The cursor is placed on the frequency with the FREQ Softkey and l ...

  • Garmin G1000H - page 125

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 113 A UDIO P ANEL AND CNS While enroute, NA V frequencies can also be auto-tuned fr om the NRST–Nearest Airports, WPT–AirportInformation, WPT–VORInformation, and NRST–NearestFrequencies ...

  • Garmin G1000H - page 126

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 114 A UDIO P ANEL AND CNS A UT O-TUNING NA V FREQUENCIES ON APPRO ACH A CTIV A TION NOTE: The primary NA V frequency is auto-tuned upon loading a VOR or ILS/Localizer approach. NOTE: When an ILS/LOC approach has been activated while navigating by GPS , the system automatical ...

  • Garmin G1000H - page 127

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 115 A UDIO P ANEL AND CNS MARKER BEA CON RECEIVER (OPTIONAL) NOTE: T he mark er beacon indicators operate independently of mark er beacon audio and cannot be turned off . Themarker beaconreceiveris usedas partof theILS. Themarker bea ...

  • Garmin G1000H - page 128

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 116 A UDIO P ANEL AND CNS DME TUNING (OPTIONAL) NOTE: When another auxiliary window is turned on, the DME T uning Window is replaced on the PFD . NOTE: When turning on the system for use, the system remembers the last frequency used for DME tuning and the NA V1 , NA V2, or H ...

  • Garmin G1000H - page 129

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 117 A UDIO P ANEL AND CNS 4.4 GTX 33 MODE S TRANSPONDER TheGTX33ModeST ransponderprovidesModeA,ModeC,and Mode S interr ogation and reply capabilities. Selective addressing or Mode Select (Mode S) capability includes the following features: ...

  • Garmin G1000H - page 130

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 118 A UDIO P ANEL AND CNS Figure 4-30 T ransponder Softkeys (PFD) Pressing the BACK Softkey returns to the top-level softkeys. ALERTS ALERTS BA CK BKSP IDENT 7 6 5 4 3 2 1 0 STBY ON AL T VFR CODE IDENT BA CK XPDR IDENT Pressing the BACK Softkey returns to the mode selection ...

  • Garmin G1000H - page 131

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 119 A UDIO P ANEL AND CNS ST ANDBY MODE (MANUAL) NOTE: In Standby Mode, the IDENT function is inoperative . Standby Mode can be selected at any time by pressing the STBY Softkey .In Standby ,thetransponder does not reply to interrogations, ...

  • Garmin G1000H - page 132

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 120 A UDIO P ANEL AND CNS AL TITUDE MODE (A UT OMA TIC OR MANU AL) Altitude Mode is automatically selected when the aircraft becomes airborne. Altitude Mode may also be selected manually by pressing the A LT Softkey . IfAltitude Modeis selected,a greenAL ...

  • Garmin G1000H - page 133

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 121 A UDIO P ANEL AND CNS ENTERING A TRANSPONDER CODE Entering a transponder code with softkeys: 1) Press the XPDR Softk ey to display the T r ansponder Mode Selection Softkeys . 2) Press the CODE Softk ey to display the T r ansponder Code Selection Softkeys , for digit entr ...

  • Garmin G1000H - page 134

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 122 A UDIO P ANEL AND CNS VFR CODE The VFR code can be entered either manually or by pressing the XPDR Softkey , then the VFR Softkey . Whenthe VFR Softkey ispr essed,thepr e-programmed VFRcodeis automatically ...

  • Garmin G1000H - page 135

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 123 A UDIO P ANEL AND CNS 4.5 ADDITIONAL AUDIO P ANEL FUNCTIONS POWER-UP The Audio Panel performs a self-testduring power -up. During the self-testall Audio Panel annunciator lights illuminateforapproximatelytwos ...

  • Garmin G1000H - page 136

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 124 A UDIO P ANEL AND CNS INTERCOM MODES NOTE: In the following modes the copilot position is configured as crew . NOTE: In the default ICS configuration, only the pilot and copilot positions can hear aircraft alerts . NOTE: When in Split-COM mode , the copilot will only h ...

  • Garmin G1000H - page 137

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 125 A UDIO P ANEL AND CNS P assengeR /c Rew i sOla te m ODe In ‘Passenger/Crew Isolate’ mode the Pilot and Copilot hear the air craft audio and each other .  The Passengers hear each other . ICS K eys Mode Operation Airc ...

  • Garmin G1000H - page 138

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 126 A UDIO P ANEL AND CNS P ilO t & c OPilO t i sOla te m ODe In ‘Pilot & Copilot Isolate’ mode the Pilot, Copilot, and Passengers hear the aircraft audio.  The Passengers hear each other . The Copilot has the ...

  • Garmin G1000H - page 139

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 127 A UDIO P ANEL AND CNS INTERCOM V OLUME AND SQUELCH The VOL/CRSR Knob controls selection and volume or manual inter com squelch adjustment for audio sources that may not be adjustable anywher e else in the system. The small knob controls the volume or squelch. T urning th ...

  • Garmin G1000H - page 140

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 128 A UDIO P ANEL AND CNS Selecting any button other than PILOT , COPL T , P ASS , MUSIC or will cancel Blue-Select Mode. Pressing the small knob will also cancel Blue-Select Mode.  After approximately ten seconds with no input ...

  • Garmin G1000H - page 141

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 129 A UDIO P ANEL AND CNS CLEARANCE RECORDER AND PLA YER (OPTIONAL) The Audio Panel contains a digital clearance recor der that recor ds up to 2.5 minutes of the selected COM radiosignal. RecordedCOMaudio? ...

  • Garmin G1000H - page 142

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 130 A UDIO P ANEL AND CNS SPLIT COM NOTE: Split COM performance is affected by the distance between the COM antennas and the separation of the tuned frequencies . If the selected COM frequencies are too close together , interference may be heard during transmission on the ot ...

  • Garmin G1000H - page 143

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 131 A UDIO P ANEL AND CNS 3D A UDIO 3D Audio is useful when multiple audio sources are present.  By using different responses in each ear , 3D audio processing cr eates the illusion that each audio source is coming fr ...

  • Garmin G1000H - page 144

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 132 A UDIO P ANEL AND CNS Symptom(s) Cause(s) Solution(s) “3D audio left” message heard in both ears . “3D audio right” message not heard 1) Mono headset in use 1) Use a stereo headset 2) Stereo headset in use with mono/stereo switch set to ‘mono’ 2) Set mono/ste ...

  • Garmin G1000H - page 145

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 133 A UDIO P ANEL AND CNS V OICE RECOGNITION V oice Recognition allows the pilot (and optionally copilot) to control the GMA 350H using spoken commands.  T o activate V oice Recognition, push and hold the Push-T o-Command (P ...

  • Garmin G1000H - page 146

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 134 A UDIO P ANEL AND CNS Control Spoken Command Action Confirmation of Action “T elephone” or “Phone” or “Jack” T oggles T elephone/Jack Illuminate/Extinguish Annunciator “T elephone mute” or “Phone mute” or “Jack mute”or “Mute telephone” or “ ...

  • Garmin G1000H - page 147

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 135 A UDIO P ANEL AND CNS Control Spoken Command Action Confirmation of Action Manual Squelch “Manual squelch” or “Man squelch” T oggles manual squelch Illuminate/Extinguish MAN SQ Annunciator “Manual squelch threshold up” or “Manual squelch volume up” or ? ...

  • Garmin G1000H - page 148

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 136 A UDIO P ANEL AND CNS Control Spoken Command Action Confirmation of Action Cursor “Cursor off” or “Cursor cancel” or “Cancel cursor” Cancels cursor when cursor is flashing Cursor is removed 3D Audio “T hree-D audio” Enables 3D audio V oice Response: “ ...

  • Garmin G1000H - page 149

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 137 A UDIO P ANEL AND CNS 4.6 A UDIO P ANEL PREFLIGHT PROCEDURE NOTE: If the pilot and/or copilot are using headsets that have a high/low switch or volume control knob , verify that the switch is in the high position and the volume control on the headsets are at maximum volu ...

  • Garmin G1000H - page 150

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 138 A UDIO P ANEL AND CNS 4.7 ABNORMAL OPERA TION Abnormal operation of the system includes equipment failures of the system components and failure of associatedequipment,includingswitchesandexternaldevices. STUCK MICROPHONE If the push-to-talk (PT ...

  • Garmin G1000H - page 151

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 139 FLIGHT MANA GEMENT SECTION 5 FLIGHT MANA GEMENT 5.1 INTRODUCTION The G1000H is an integrated flight, engine, communication, navigation and surveillance system. This section of the Pilot’ s Guide explains flight management using the G1000H. The most prominent part of ...

  • Garmin G1000H - page 152

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 140 FLIGHT MANA GEMENT Figure 5-1 GPS Navigation Information on the PFD Location of: - Inset Map - Direct T o W indow - Flight Plan Window - Procedures Window - Nearest Airports Window Navigation Status Box Navigation Mode Figure 5-2 GPS Navigation Information on the MFD Nav ...

  • Garmin G1000H - page 153

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 141 FLIGHT MANA GEMENT • Active ight plan leg(e.g., ‘D-> KICT’ or ‘KIXD-> KCOS’) or  ight plan annunciations (e.g., ‘T urn right to 021˚ in 8 seconds’) • Distance (DIS) and Bearing ...

  • Garmin G1000H - page 154

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 142 FLIGHT MANA GEMENT 5.2 USING MAP DISPLA YS Map displays are used extensively in the system to pr ovide situational awareness in flight. Most system maps can display the following information: • Airports, NA V AIDs, airspaces, airways, land data (h ...

  • Garmin G1000H - page 155

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 143 FLIGHT MANA GEMENT NOTE: When panning or reviewing active flight plan legs in a non-North Up orientation, the map does not show the map orientation nor the wind direction and speed. NOTE: Map orientation can only be changed on the Navigation Map P age . Any other displa ...

  • Garmin G1000H - page 156

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 144 FLIGHT MANA GEMENT MAP RANGE There are 28 dif ferent map ranges available, fr om 500 feet to 2000 nm. The current range is indicated in the lower right corner of the map and represents the top-to-bottom distance covered by the map. When the map range is decreased to a po ...

  • Garmin G1000H - page 157

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 145 FLIGHT MANA GEMENT • The ‘time out’ time (congurable on the Map Setup Page for the Map Group) determines how long auto zoom is overridden by a manual adjustment of the range knob. At the expiration of this ...

  • Garmin G1000H - page 158

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 146 FLIGHT MANA GEMENT MAP P ANNING Map panning allows the pilot to: • Viewpartsofthemapoutsidethedisplayedrangewithoutadjustingthemaprange • Highlightandselectlocationsonthemap • Reviewinformation ...

  • Garmin G1000H - page 159

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 147 FLIGHT MANA GEMENT When the Map Pointer is placed on an object, the name of the object is highlighted (even if the name was not originally displayed on the map). When any map feature or object is selected on the map display , pertinent information is displayed. Figure 5- ...

  • Garmin G1000H - page 160

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 148 FLIGHT MANA GEMENT When the Map Pointer crosses an airspace boundary , the boundary is highlighted and airspace information is shown at the top of the display . The information includes the name and class of airspace, the ceiling in feet above Mean Sea Level (MSL), and t ...

  • Garmin G1000H - page 161

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 149 FLIGHT MANA GEMENT Reviewing information for an airport, NA V AID , or user waypoint: 1) Place the Map P ointer on a waypoint. 2) Press the ENT K ey to display the W aypoint Information P age for the selected waypoint. 3) Press the GO B ACK Softk ey , the CLR K ey , or t ...

  • Garmin G1000H - page 162

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 150 FLIGHT MANA GEMENT Viewing air space information for a special-use or controlled airspace: 1) Place the Map P ointer on an open area within the boundaries of an airspace . 2) Press the ENT K ey to display an options menu. 3) ‘Review Airspaces’ should already be highl ...

  • Garmin G1000H - page 163

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 151 FLIGHT MANA GEMENT MEASURING BEARING AND DIST ANCE Distance and bearing from the air craft’ s present position to any point on the viewable navigation map may be calculated using the ‘Measure Bearing and Distance’ selection fr om Navigati ...

  • Garmin G1000H - page 164

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 152 FLIGHT MANA GEMENT T OPOGRAPHY All navigation maps can display various shades of topography colors representing land elevation, similar to aviation sectional charts. T opographic data can be displayed or removed as described in the following procedur es. Navigation Map B ...

  • Garmin G1000H - page 165

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 153 FLIGHT MANA GEMENT Figure 5-15 Navigation Map Setup Menu - T OPO DA T A Setup TOPO DA T A On/Off TOPO DA T A Range The topographic data range is the maximum map range on which topographic data is displayed. NOTE: Since the PFD Inset Map is much smaller than the MFD navig ...

  • Garmin G1000H - page 166

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 154 FLIGHT MANA GEMENT Figure 5-16 Navigation Map - T OPO SCALE Maximum Displayed Elevation Minimum Displayed Elevation Aircraft Altitude (MSL) Ground Elevation at Map Pointer Location (only visible when Map Pointer is displayed) Range of Displayed Elevations Displaying/remo ...

  • Garmin G1000H - page 167

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 155 FLIGHT MANA GEMENT MAP SYMBOLS This section discusses the types of land and aviation symbols that can be displayed. Each listed type of symbol can be turned on or off, and the maximum range to display each symbol can be set. The decluttering of the symbols from the map u ...

  • Garmin G1000H - page 168

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 156 FLIGHT MANA GEMENT A VIA TION SYMBOLS The following items are configured on the aviation menu: A viation Symbols (T ext label size can be None, Small, Medium (Med), or Large (Lrg)) Symbol Default Range (nm) Maximum Range (nm) Active Flight Plan Leg (ACTIVE FPL) 2000 200 ...

  • Garmin G1000H - page 169

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 157 FLIGHT MANA GEMENT SYMBOL SETUP All pages with maps can display land symbols (roads, lakes, bor ders, etc). Land symbols can be removed totally (turned off). Displaying/removing all land symbols: 1) Press the MENU K ey with the Navigation Map P age displayed. T he P age ...

  • Garmin G1000H - page 170

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 158 FLIGHT MANA GEMENT 10) Press the FMS Knob to return to the Navigation Map P age . Figure 5-19 Navigation Map Setup Menu - LAND GROUP Setup Maximum Display Range T ext Label Size (None, Small, Med, or Lrg) Figure 5-20 Navigation Map Setup Menu - A VIA TION GROUP Setup Max ...

  • Garmin G1000H - page 171

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 159 FLIGHT MANA GEMENT MAP DECLUTTER The declutter feature allows the pilot to pr ogressively step through four levels of r emoving map information. The declutter level is displayed in the DCL TR Softkey and next to the Declutter Menu Option. Figure 5-21 Navigation Map - Dec ...

  • Garmin G1000H - page 172

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 160 FLIGHT MANA GEMENT T able 5-3 lists the items displayed at each declutter level.  The ‘X’ represents map items displayed for the various levels of declutter . Item No Declutter Declutter -1 Declutter -2 Declutt ...

  • Garmin G1000H - page 173

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 161 FLIGHT MANA GEMENT AIRW A YS This airways discussion is based upon the North American airway structure. The airway structure in places other than North America vary by location, etc. and are not discussed in this book. Low Altitude Airways (or Victor Airways) primarily s ...

  • Garmin G1000H - page 174

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 162 FLIGHT MANA GEMENT Airways may be displayed on the map at the pilot’ s discretion using either a combination of AIR W A YS Softkey presses, or menu selections using the MENU Key fr om the Navigation Map Page. The Air way range can also be programmed to only display Air ...

  • Garmin G1000H - page 175

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 163 FLIGHT MANA GEMENT The following range items are configurable on the airways menu: Airway T ype Symbol Default Range (nm) Maximum Range (nm) Low Altitude Airway (LOW AL T AIRWA Y) 200 500 High Altitude Airway (HI AL T AIRWA Y) 300 500 T able 5-4 Airway Range Information ...

  • Garmin G1000H - page 176

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 164 FLIGHT MANA GEMENT Figure 5-25 Navigation Map Setup Menu -TRA CK VECT OR, WIND VECT OR, NA V RANGE RING , FUEL RANGE RING Setup T rack V ector - On/Off - Look Ahead Time Fuel Range - On/Off - Fuel Reserve Time Wind V ector On/Off Nav Range Ring On/Off WIND VECT OR The ma ...

  • Garmin G1000H - page 177

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 165 FLIGHT MANA GEMENT NA V RANGE RING The Nav Range Ring shows the direction of travel (gr ound track) on a rotating compass car d. The range is determined by the map range. The range is 1/4 of the map range (e.g., 37.5 nm on a 150 nm map). Figure 5-27 Navigation Map - Nav ...

  • Garmin G1000H - page 178

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 166 FLIGHT MANA GEMENT FUEL RANGE RING The map can display a fuel range ring which shows the remaining flight distance. A dashed green cir cle indicates the selected range to reserve fuel. A solid green circle indicates the total endurance range. If only reserve fuel remain ...

  • Garmin G1000H - page 179

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 167 FLIGHT MANA GEMENT FIELD OF VIEW (SVS) The map can display the boundaries of the PFD Synthetic Vision System (SVS) lateral field of view . The field of view is shown as two dashed lines forming a V shape in front of the air craft symbol on the map. Figure 5-29 Navigati ...

  • Garmin G1000H - page 180

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 168 FLIGHT MANA GEMENT SELECTED AL TITUDE INTERCEPT ARC The map can display the location along the current track wher e the aircraft will inter cept the selected altitude. The location will be shown as a light blue arc when the air craft is actuallly climbing or descending. ...

  • Garmin G1000H - page 181

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 169 FLIGHT MANA GEMENT 5.3 W A YPOINTS W aypoints are pr edetermined geographical positions (internal database) or pilot-entered positions, and are used for all phases of flight planning and navigation. Communication and navigation frequenciescan be tuned? ...

  • Garmin G1000H - page 182

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 170 FLIGHT MANA GEMENT Figure 5-32 W aypoint Information Window - Duplicate Identifier Duplicate Message Identifier with Duplicates Duplicate Waypoints AIRPORTS NOTE: ‘North Up’ orientation on the Airport Information P age cannot be changed; the pilot needs to be aware ...

  • Garmin G1000H - page 183

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 171 FLIGHT MANA GEMENT Figure 5-33 Airport Information P age Airport/Runway Diagram Navigation Map Showing Selected Airport Runway Information - Designation - Length/Width/Surface - Lighting Available Airport Information - ID/Facility/City - Usage T ype/Region - Lat/Long/Ele ...

  • Garmin G1000H - page 184

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 172 FLIGHT MANA GEMENT Figure 5-34 Airport Directory P age Example Airport Information - ID/Facility/City - Usage T ype/Region Airport Directory Information Softkeys The AOP A directory information is viewed on the Airport Dir ector y Page by pressing the INFO softkey until ...

  • Garmin G1000H - page 185

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 173 FLIGHT MANA GEMENT Selecting an airport for review by identifier , facility name , or location: 1) F rom the Airport Information P age , press the FMS Knob . 2) Use the FMS Knobs and enter an identifier , facility name , or location. 3) Press the ENT Ke y. 4) Press the ...

  • Garmin G1000H - page 186

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 174 FLIGHT MANA GEMENT Figure 5-35 Nearest Airports Window on PFD COM Freq. Info. - Identification - Frequency Airport Identifier/ T ype Length of Longest Runway Approach Available Additional Airports (within 200 nm) NRST Softkey Bearing/Distance to Airport Pressing the EN ...

  • Garmin G1000H - page 187

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 175 FLIGHT MANA GEMENT If there are no items for display in a boxed ar ea, text indicating that fact is displayed. The currently selected airport remains in the list until it is unselected. Figure 5-37 Nearest Airport P age Nearest Airport Navigation Map Showing Nearest Airp ...

  • Garmin G1000H - page 188

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 176 FLIGHT MANA GEMENT Viewing runway information for a specific airport: 1) With the Nearest Airports P age displayed, press the RNWY Softk ey; or press the MENU K ey , highlight ‘Select Runway Window’; and press the ENT K ey . T he cursor is placed in the ‘R UNWA Y ...

  • Garmin G1000H - page 189

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 177 FLIGHT MANA GEMENT INTERSECTIONS NOTE: The V OR displayed on the Intersection Information P age is the nearest VOR, not necessarily the VOR used to define the intersection. The Intersection Information Page is used to view information about intersections. In addition to ...

  • Garmin G1000H - page 190

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 178 FLIGHT MANA GEMENT NOTE: The list only includes w aypoints that are within 200 nm. Figure 5-40 Nearest Inter sections P age Nearest Intersection Navigation Map Showing Nearest Intersection Intersection Information - Identifier/Symbol - Bearing/Distance to intersection f ...

  • Garmin G1000H - page 191

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 179 FLIGHT MANA GEMENT NDB S The NDB Information Page is used to view information about NDBs. In addition to displaying a map of the currently selected NDB and surr ounding area, the page displays NDB information in four boxes labeled ‘NDB’,‘INFORMA TION’,‘FR ...

  • Garmin G1000H - page 192

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 180 FLIGHT MANA GEMENT TheNearestNDB Pagecan beused toquicklynd aNDB closeto theightpath. In additionto displaying a map of the surrounding ar ea, the page displays information for up to 25 nearest NDBs ...

  • Garmin G1000H - page 193

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 181 FLIGHT MANA GEMENT VO R S The VOR Information Page can be used to view information about VOR and ILS signals (since ILS signals can be r eceived on aNA V receiver), or to quicklyauto-tune a VOR or ILS frequency .  Locali ...

  • Garmin G1000H - page 194

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 182 FLIGHT MANA GEMENT 2) Highlight ‘Select VOR Window’, and press the ENT Ke y. 3) Press the ENT K ey or turn either FMS Knob to select an identifier in the Nearest VOR Bo x. 4) Press the FMS Knob to remove the flashing cursor . The Nearest VOR Page can ...

  • Garmin G1000H - page 195

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 183 FLIGHT MANA GEMENT USER W A YPOINTS The system can create and store up to 1,000 user -defined waypoints. User waypoints can be created fr om any mappage(except PFDInsetMap,AUX-T rip PlanningPage,orProcedurePages)byselecting a ...

  • Garmin G1000H - page 196

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 184 FLIGHT MANA GEMENT Figure 5-46 Nearest User W aypoint P age Selected User Waypoint Navigation Map Showing Selected User Waypoint Nearest User Wpt List - Identifier - Bearing/Distance from aircraft position User Waypoint Info - Comment - Lat/Long Reference Wpt Info - Ide ...

  • Garmin G1000H - page 197

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 185 FLIGHT MANA GEMENT 1) Press the FMS Knob to activate the cursor . 2) Enter a user waypoint name (up to six char acters). 3) Press the ENT K ey . T he message ‘ Are you sure you want to create the new User W aypoint AAAAAA?’ is displayed. 4) With ‘YES’ highlighted ...

  • Garmin G1000H - page 198

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 186 FLIGHT MANA GEMENT 3) Enter a user waypoint name (up to six char acters). 4) Press the ENT K ey to accept the selected name . T he first reference waypoint bo x is highlighted. 5) If desired, define the type and location of the waypoint in one of the following w ays: a ...

  • Garmin G1000H - page 199

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 187 FLIGHT MANA GEMENT Changing the location of an existing waypoint to the aircraft pr esent position: 1) Enter a waypoint name or select the w aypoint in the User W aypoint List, then press the ENT K e y. 2) Press the MENU Ke y. 3) Select ‘Use Present P osition’. 4) Pr ...

  • Garmin G1000H - page 200

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 188 FLIGHT MANA GEMENT DELETING USER W A YPOINTS Deleting a single user waypoint: 1) Highlight a User W aypoint in the User W aypoint List, or enter a waypoint in the User W aypoint field. 2) Press the DELETE Softk ey or press the CLR K ey . ‘Y es’ is highlighted in the ...

  • Garmin G1000H - page 201

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 189 FLIGHT MANA GEMENT 5.4 AIRSP ACES The system can display the following types of airspaces: Class B/TMA, Class C/TCA, Class D, Restricted, MOA (Military), Other Airspace, Air Defense Interdiction Zone (ADIZ), and T emporary Flight Restriction (TFR). Figure 5-48 Airspaces ...

  • Garmin G1000H - page 202

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 190 FLIGHT MANA GEMENT The Airspace Alerts Box allows the pilot to turn the controlled/special-use airspace message alerts on or of f. This does not affect the alerts listed on the Near est Airspaces Page or the airspace boundaries depicted on the Navigation Map Page. It sim ...

  • Garmin G1000H - page 203

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 191 FLIGHT MANA GEMENT Map ranges for the airspace boundaries are selected fr om the A viation Group in the Map Setup Menu. See T able 5-2 for the default and maximum ranges for each type of airspace and the symbol used to define the airspace area. The Nearest Airspac ...

  • Garmin G1000H - page 204

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 192 FLIGHT MANA GEMENT Pressing the PFD ALER TS Softkey displays the message window on the PFD. The following airspace alerts are displayed in the message window: Message Comments INSIDE ARSPC – Inside airspace . T he aircraft is inside the airspace . ARSPC AHEAD – Airsp ...

  • Garmin G1000H - page 205

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 193 FLIGHT MANA GEMENT 5.5 DIRECT -T O-NA VIGA TION The Direct-to method of navigation, initiated by pressing the Dir ect-to Key on either the MFD or PFD, is quickertousethanaightplanwhenthedesireistonavigatetoasinglepoint? ...

  • Garmin G1000H - page 206

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 194 FLIGHT MANA GEMENT Figure 5-52 Direct-to Window - PFD Direct-to Point Info - Identifier/Symbol/City - Facility Name Activation Command Direct-to Point Info - Bearing/Distance - Desired Course VNV Constraints - Altitude at Arrival - Along T rack Offset Any waypoint can b ...

  • Garmin G1000H - page 207

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 195 FLIGHT MANA GEMENT 3) Select the desired waypoint. 4) Press the ENT K ey . T he cursor is now displayed on ‘ ACTIV A TE?’. 5) Press the ENT K ey again to activate the direct-to . Or : 1) Select the Active Flight Plan P age on the MFD , or the Active Flight Plan Windo ...

  • Garmin G1000H - page 208

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 196 FLIGHT MANA GEMENT 4) Press the ENT K ey . T he cursor is now displayed on ‘ ACTIV A TE?’. 5) Press the ENT K ey again to activate the direct-to . Direct-to destinations may also be selected by using the pointer on the navigation map pages. If no airport, NA V AID,? ...

  • Garmin G1000H - page 209

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 197 FLIGHT MANA GEMENT When navigating a direct-to, the system sets a direct gr eat circle course to the selected destination. The course toadestinationcanalsobemanuallyselectedusingthecourseeld(‘COURSE’)ontheDirect-toW ...

  • Garmin G1000H - page 210

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 198 FLIGHT MANA GEMENT Removing a VNV altitude constraint: 1) Press the Direct-to K ey to display the Direct-to Window . 2) Press the MENU Ke y. 3) With ‘Clear V ertical Constraints’ highlighted, press the ENT K e y. Figure 5-55 Direct-to Window - Clearing V ertical Cons ...

  • Garmin G1000H - page 211

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 199 FLIGHT MANA GEMENT 5.6 FLIGHT PLANNING Flight planning on the system consists of building a flight plan by entering waypoints one at a time, adding waypoints along airways, and inserting departures, airways, arrivals, or approaches as needed. The system allows flight p ...

  • Garmin G1000H - page 212

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 200 FLIGHT MANA GEMENT The following could cause the airway update to fail: • Airwayidentier ,entrywaypointorexitwaypointnotfoundinthenewdatabase. • Airway entry/exitwaypoint isnot anacceptable waypoint ...

  • Garmin G1000H - page 213

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 201 FLIGHT MANA GEMENT Active Flight Plan Comment Figure 5-57 Active Flight Plan Window on PFD Active Flight Plan Leg Active Flight Plan Waypoint List - Waypoint ID - Desired T rack to Waypoint - Distance to Waypoint - Airway Identifier Figure 5-58 Flight Plan Catalog P age ...

  • Garmin G1000H - page 214

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 202 FLIGHT MANA GEMENT 4) Enter the identifier , facility , or city name of the departure waypoint or select a w aypoint from the submenu of waypoints and press the ENT K ey . T he active flight plan is modified as each waypoint is entered. 5) Repeat step numbers 3 and 4 ...

  • Garmin G1000H - page 215

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 203 FLIGHT MANA GEMENT Flight plans can be imported from an SD Car d or exported to an SD Card fr om the Stored Flight Plan Page. Importing a Flight Plan from an SD Card 1) Insert the SD card containing the flight plan in the top card slot on the MFD . 2) Press the FPL K ey ...

  • Garmin G1000H - page 216

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 204 FLIGHT MANA GEMENT NO TE: If the imported flight plan contains a w aypoint with a name that duplicates the name of a waypoint already stored on the system, the system compares the coordinates of the imported waypoint with those of the existing waypoint. If the coordinat ...

  • Garmin G1000H - page 217

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 205 FLIGHT MANA GEMENT ADDING W A YPOINTS TO AN EXISTING FLIGHT PLAN W aypoints can be added to the active flight plan or any stored flight plan. Choose the flight plan, select the desired point of insertion, enter the waypoint, and it is added in fr ont of the selected w ...

  • Garmin G1000H - page 218

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 206 FLIGHT MANA GEMENT 3) Press the EDIT Softk ey; or press the ENT K ey , turn the large FMS Knob clockwise to select “EDIT” and press the ENT K ey . T he Stored Flight Plan P age is displayed. 4) Select the point in the flight plan to add the new waypoint. T he new wa ...

  • Garmin G1000H - page 219

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 207 FLIGHT MANA GEMENT Creating and adding user waypoints to the active flight plan: 1) Press the Joystick to activate the panning function on the Active Flight Plan P age and pan to the map location of the desired user waypoint. 2) Select the LD WPT Softk ey; or press the ...

  • Garmin G1000H - page 220

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 208 FLIGHT MANA GEMENT 5) T urn the FMS Knob to select the desired airw ay from the list, and press the ENT K ey . Low altitude airw ays are shown first in the list, followed by “all” altitude airways , and then high altitude airways . 6) T urn the FMS Knob to select th ...

  • Garmin G1000H - page 221

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 209 FLIGHT MANA GEMENT RESTRICTIONS ON ADDING AIRW A Y S Some airways have directional restrictions on all or part of the r oute. Air way “A2” in Eur ope has a directional restriction over the whole r oute such that it can be flown only in the direction MTD-ABB-BNE-DEV ...

  • Garmin G1000H - page 222

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 210 FLIGHT MANA GEMENT DEP ARTURE (DP) A Departure Pr ocedure (DP) is loaded at the departure airport in the flight plan. Only one departure can be loaded at a time in a flight plan. The route is defined by selection of a departur e, the transition waypoints, and a runway ...

  • Garmin G1000H - page 223

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 211 FLIGHT MANA GEMENT Figure 5-69 Departure Loading P age - Selecting T ransition Departure Airport Selected Departure Departure T ransition Points Available Selected Runway Selected Departure End Point Preview of Selected Departure Selected T ransition Figure 5-70 Stored F ...

  • Garmin G1000H - page 224

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 212 FLIGHT MANA GEMENT ARRIV AL (ST AR) A Standar d T erminal Arrival (ST AR) is loaded at the destination airport in the flight plan. Only one arrival can be loaded at a time in a flight plan. The route is defined by selection of an arrival, the transition waypoints, and ...

  • Garmin G1000H - page 225

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 213 FLIGHT MANA GEMENT Figure 5-72 Arrival Loading P age - Selecting the T ransition Destination Airport Selected Arrival T ransitions Available with DBRY1 Arrival Waypoint Sequence Preview of Selected Arrival Selected T ransition Figure 5-73 Stored Flight Plan P age - Arriv ...

  • Garmin G1000H - page 226

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 214 FLIGHT MANA GEMENT APPRO ACH (APPR) An Approach Pr ocedure (APPR) can be loaded at any airport that has an appr oach available. Only one approach can be loaded at a time in a flight plan. The r oute for a selected approach is defined by designating transition waypoints ...

  • Garmin G1000H - page 227

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 215 FLIGHT MANA GEMENT Figure 5-75 Approach Loading P age - Selecting the T ransition Destination Airport Selected Approach T ransitions Available with Selected Approach Approach Waypoint Sequence Preview of Selected Approach Load Approach? Selected T ransition Barometric Mi ...

  • Garmin G1000H - page 228

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 216 FLIGHT MANA GEMENT FLIGHT PLAN ST ORA GE The system can store up to 99 flight plans, numbered 1 thr ough 99. The active flight plan is erased when the system is powered of f or when another flight plan is activated. Details about each stored flight plan can be viewed ...

  • Garmin G1000H - page 229

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 217 FLIGHT MANA GEMENT A CTIV A TE A FLIGHT PLAN Activating a stored flight plan erases the active flight plan and replaces it with the flight plan being activated. Inverting a stored flight plan reverses the waypoint or der , erases the active flight plan, and replaces ...

  • Garmin G1000H - page 230

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 218 FLIGHT MANA GEMENT 3) Select the DELETE Softk ey; press the CLR K ey; or press the MENU K ey , highlight ‘Delete Flight Plan’, and press the ENT K ey . T he ‘Delete Flight Plan XX?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key to delete th ...

  • Garmin G1000H - page 231

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 219 FLIGHT MANA GEMENT 4) With ‘OK’ highlighted, press the ENT K ey . T o cancel the request, press the CLR K ey , or highlight ‘CANCEL ’ and press the ENT Ke y. 5) Press the FMS Knob to remove the flashing cursor . Deleting an entire airway from the active flight ...

  • Garmin G1000H - page 232

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 220 FLIGHT MANA GEMENT 7) With ‘OK’ highlighted, press the ENT K ey . T o cancel the request, press the CLR K ey , or highlight ‘CANCEL ’ and press the ENT Ke y. 8) Press the FMS Knob to remove the flashing cursor . Deleting an entire airway from a stor ed flight p ...

  • Garmin G1000H - page 233

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 221 FLIGHT MANA GEMENT 7) With ‘OK’ highlighted, press the ENT K ey . T o cancel the request, press the CLR K ey , or highlight ‘CANCEL ’ and press the ENT Ke y. 8) Press the FMS Knob to remove the flashing cursor . CHANGING FLIGHT PLAN COMMENTS (NAMES) The comment ...

  • Garmin G1000H - page 234

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 222 FLIGHT MANA GEMENT An along track of fset distance cannot be modified once entered. If the along track offset distance must be changed, the existing along track of fset waypoint must be deleted and a new one created with the new of fset distance. Figure 5-78 Along T rac ...

  • Garmin G1000H - page 235

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 223 FLIGHT MANA GEMENT P ARALLEL TRA CK The Parallel T rack (PTK) feature allows creation of a parallel course of fset of 1 to 50 nm left or right of the current flight plan. When Parallel T rack is activated, the course line drawn on the map pages shows the parallel course ...

  • Garmin G1000H - page 236

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 224 FLIGHT MANA GEMENT Figure 5-80 P arallel T rack Window Offset Direction Offset Distance Activation Prompt Figure 5-81 P arallel T rack Active Parallel T rack Waypoints - TIFTO-p - TOP-p - SLN-p - HYS-p - LAA-p Activating Parallel T rack affects the entire active flight ...

  • Garmin G1000H - page 237

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 225 FLIGHT MANA GEMENT If the parallel track proposed by the of fset direction and distance is not allowed by the system, the activation prompt is displayed, but disabled. Parallel T rack cannot be activated if a course is set using direct-to or if the active leg is the fir ...

  • Garmin G1000H - page 238

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 226 FLIGHT MANA GEMENT A CTIV A TING A FLIGHT PLAN LEG The system allows selection of a highlighted leg as the “active leg” (the flight plan leg which is currently used for navigation guidance). Activating a flight plan leg: 1) Press the FPL K ey to display the Active ...

  • Garmin G1000H - page 239

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 227 FLIGHT MANA GEMENT Figure 5-85 Active Flight Plan P age - New Active Leg New Active Flight Plan Leg Confirmation Window INVERTING A FLIGHT PLAN Any flight plan may be inverted (reversed) for navigation back to the original departure point. Inverting the active flight ...

  • Garmin G1000H - page 240

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 228 FLIGHT MANA GEMENT FLIGHT PLAN VIEWS Information about flight plans can be viewed in more than one way . The active flight plan can be configured to show cumulative distance over the length of the flight plan or the distance for each leg of the flight plan; and the ...

  • Garmin G1000H - page 241

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 229 FLIGHT MANA GEMENT Figure 5-87 Active Flight Plan - Wide vs . Narrow View WIDE Softkey , NARROW Softkey , LEG-LEG Softkey , CUM Softkey Active Flight Plan Narrow View Active Flight Plan Wide View COLLAPSING AIRW A Y S The system allows airways on the active flight plan ...

  • Garmin G1000H - page 242

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 230 FLIGHT MANA GEMENT Figure 5-88 Expanded/Collapsed Airways Q3.FEPOT Airway Collapsed View Expanded View Collapsing/expanding the airways in the active flight plan: 1) Press the FPL K ey to display the Active Flight Plan P age (MFD) or the Active Flight Plan Window (PFD). ...

  • Garmin G1000H - page 243

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 231 FLIGHT MANA GEMENT 5.7 VERTICAL NA VIGA TION NOTE: T he system supports vertical navigation for all lateral leg types except for CA, CI, F A, FM, HA, HM, PI, V A, VD , VI, VR, and VM. Vertical constraints are not retained in stored flight plans . The system system V ert ...

  • Garmin G1000H - page 244

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 232 FLIGHT MANA GEMENT Cancelingverticalnavigationresultsinverticaldeviation (VDEV),verticalspeedrequired(VSREQ),andtime to top of descent/bottom of descent (TIME TO TOD/BOD) going invalid. The V ertical Deviation Indicator (VD ...

  • Garmin G1000H - page 245

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 233 FLIGHT MANA GEMENT 4) Press the ENT K ey . V ertical guidance begins to the altitude constraint for the selected w aypoint. 5) Press the FMS Knob to remove the flashing cursor . The vertical navigation profile can be modified by dir ectly entering a vertical speed tar ...

  • Garmin G1000H - page 246

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 234 FLIGHT MANA GEMENT White T ext Light Blue T ext Light Blue Subdued T ext Large T ext Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point. T his altitude is provided as a reference and is not designated to be us ...

  • Garmin G1000H - page 247

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 235 FLIGHT MANA GEMENT An altitude constraint is invalid if: • Meetingtheconstraintrequirestheair crafttoclimb • Meetingtheconstraintrequiresthemaximumightpathangleormaximumverticalspeedtobeexceed ...

  • Garmin G1000H - page 248

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 236 FLIGHT MANA GEMENT Reverting a manually entered altitude constraint back to the navigation database value: 1) Press the FPL K ey to display the Active Flight Plan P age on the MFD . 2) Press the FMS Knob , and turn to highlight the desired waypoint altitude constraint. 3 ...

  • Garmin G1000H - page 249

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 237 FLIGHT MANA GEMENT 5.8 PROCEDURES The system can access the whole range of instrument procedur es available. Departures (DPs), arrivals (ST ARs), and non-precision and pr ecision appr oaches (APPRs) are stor ed within the database and can be loaded using the Procedur es ...

  • Garmin G1000H - page 250

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 238 FLIGHT MANA GEMENT Figure 5-92 Departure Selection Departure Airport Departure Preview Available Procedure Actions Departure Choices Loaded Procedures Procedure Loading Page Selection Softkeys Figure 5-93 Departure Loading Loaded Departure Selected Departure ...

  • Garmin G1000H - page 251

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 239 FLIGHT MANA GEMENT Viewing available departur es at an airport: 1) F rom the Airport Information P age (first page in the WPT group), select the DP Softk ey . T he Departure Information P age is displayed, defaulting to the airport displayed on the Airport information P ...

  • Garmin G1000H - page 252

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 240 FLIGHT MANA GEMENT ARRIV ALS A Standar d T erminal Arrival (ST AR) can be loaded at any airport that has one available. Only one arrival can be loaded at a time in a flight plan. If an arrival is loaded when another arrival is already in the active flight plan, the new ...

  • Garmin G1000H - page 253

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 241 FLIGHT MANA GEMENT Figure 5-95 Arrival Loading Loaded Arrival Selected Arrival Procedure Loading Page Selection Softkeys Viewing available arrivals at an airport: 1) F rom the Airport Information P age (first page in the WPT group), select the ST AR Softk ey . T he Arri ...

  • Garmin G1000H - page 254

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 242 FLIGHT MANA GEMENT REMO VING AN ARRIV AL FROM THE A CTIVE FLIGHT PLAN When plans change while flying IFR, arrivals can be easily removed fr om the Active Flight Plan. Removing an arrival from the active flight plan: 1) Press the FPL K ey to display the Active Flight Pl ...

  • Garmin G1000H - page 255

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 243 FLIGHT MANA GEMENT The system W AAS GPS allows for flying LNA V , LNA V/VNA V , and LPV approaches accor ding to the published chart. LNA V+V is a standar d LNA V approach with advisory vertical guidance provided for assistance in maintaining a constant vertical glidepa ...

  • Garmin G1000H - page 256

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 244 FLIGHT MANA GEMENT Figure 5-96 Approach Selection Destination Airport Approach Preview Available Procedure Actions Approach Choices Loaded Procedures Figure 5-97 Approach Loading Loaded Approach Selected Approach LOAD or ACTIV A TE? Annunciation Procedure Loading Page Se ...

  • Garmin G1000H - page 257

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 245 FLIGHT MANA GEMENT Viewing available appr oaches at an airport: 1) F rom the Airport Information P age (first page in the WPT group), select the APR Softk ey . The Approach Information P age is displayed, defaulting to the airport displayed on the Airport information P ...

  • Garmin G1000H - page 258

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 246 FLIGHT MANA GEMENT A CTIV A TING AN APPRO A CH A previously loaded appr oach can be activated from the Pr ocedures Window . Activating a previously loaded approach: 1) Press the PROC K ey . T he Procedures Window is displayed with ‘ Activate Approach’ highlighted. 2) ...

  • Garmin G1000H - page 259

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 247 FLIGHT MANA GEMENT MISSED APPRO ACH Activating a missed approach in the active flight plan: Press the Go Around Button. Or : Fly past the MAP , and press the SUSP Softk ey on the PFD . Or : 1) Press the PROC Ke y. 2) T urn the FMS Knob to highlight ‘ ACTIV A TE MISSED ...

  • Garmin G1000H - page 260

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 248 FLIGHT MANA GEMENT 5.9 TRIP PLANNING The system allows the pilot to view trip planning information, fuel information, and other information for a specified flight plan or flight plan leg based on automatic data, or based on manually entered data. W eight planning is a ...

  • Garmin G1000H - page 261

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 249 FLIGHT MANA GEMENT TRIP ST A TISTICS The trip statistics are calculated based on the selected starting and ending waypoints and the trip planning inputs. In flight plan mode (FPL) with a stored flight plan selected (NN), and the entire flight plan (CUM) selected, the ...

  • Garmin G1000H - page 262

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 250 FLIGHT MANA GEMENT FUEL ST A TISTICS The fuel statistics are calculated based on the selected starting and ending waypoints and the trip planning inputs. Some of the calculated trip statistics are dashed when the selected leg of the active flight plan has already been ? ...

  • Garmin G1000H - page 263

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 251 FLIGHT MANA GEMENT Selecting automatic or manual page mode: Select the AU TO Softk ey or the MANUAL Softk ey; or press the MENU K ey , highlight ‘ Auto Mode’ or ‘Manual Mode’, and press the ENT Ke y. Selecting flight plan or waypoint mode: Select the FPL Softk e ...

  • Garmin G1000H - page 264

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 252 FLIGHT MANA GEMENT 5.10 RAIM PREDICTION RAIM (Receiver Autonomous Integrity Monitoring) is a GPS receiver function that performs a consistency check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to calculate a position ...

  • Garmin G1000H - page 265

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 253 FLIGHT MANA GEMENT 5) T urn the FMS Knobs to enter an arriv al time and press the ENT Ke y. 6) T urn the FMS Knobs to enter an arriv al date and press the ENT Ke y. 7) Press the ENT K ey with ‘COMPUTE RAIM?’ highlighted to begin the computation. Predicting RAIM avail ...

  • Garmin G1000H - page 266

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 254 FLIGHT MANA GEMENT Enabling/Disabling SB AS: 1) Select the A UX-GPS Status P age . 2) Press the SB AS Softkey . 3) Press the FMS Knob , and turn the large FMS Knob to highlight ‘EGNOS’, ‘MSAS’ or ‘WAAS’. 4) Press the ENT K ey to disable SBAS . Press the ENT K ...

  • Garmin G1000H - page 267

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 255 FLIGHT MANA GEMENT 5.11 NA VIGA TING A FLIGHT PLAN The following discussion is an example of navigating a flight plan with the W AAS capable GPS system while the system provides vertical guidance thr ough descents. A lateral flight plan (LNA V) would be navigated in mu ...

  • Garmin G1000H - page 268

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 256 FLIGHT MANA GEMENT 3) A TC now assigns routing to join V4. A heading of 290º is assigned to intercept V4. T he aircraft turns to heading 290° as seen in Figure 5-106. Figure 5-106 Assigned Heading of 290º 4) Enter V4 into the flight plan. a) Press the FMS Knob to act ...

  • Garmin G1000H - page 269

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 257 FLIGHT MANA GEMENT b) T he desired entry point for V4 (T OP) must be entered. T urn the large FMS Knob to highlight the desired flight plan insertion point (SLN) as shown in Figure 5-107. When the V4 entry point (T OP) is inserted, it is placed immediately above the hig ...

  • Garmin G1000H - page 270

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 258 FLIGHT MANA GEMENT d) Press the ENT K ey . T OP is inserted into the flight plan as in Figure 5-109. Figure 5-109 T OP Inserted into the Flight Plan e) With SLN still highlighted as in Figure 5-109, turn the small FMS Knob clockwise . T he W aypoint Information P age is ...

  • Garmin G1000H - page 271

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 259 FLIGHT MANA GEMENT h) Press the ENT K ey . T he list of available exits for V4 is now displayed as in Figure 5-111. Figure 5-111 List of Available Exits for V4 i) If necessary , turn either FMS Knob to select the desired exit. In this case Salina VOR (SLN) is selected as ...

  • Garmin G1000H - page 272

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 260 FLIGHT MANA GEMENT l) V4 is now loaded into the flight plan as shown in Figure 5-113. Figure 5-113 V4 is Loaded in the Flight Plan 5) Making V4 the active leg of the flight plan. a) Press the FMS Knob to activ ate the cursor . b) T urn the large FMS Knob to highlight S ...

  • Garmin G1000H - page 273

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 261 FLIGHT MANA GEMENT d) V erify the displayed leg is the desired leg and press the ENT K ey . Note in Figure 5-115, the magenta arrow in the flight plan window and magenta line on the map indicating V4 is now the active flight plan leg. Note the phase of flight remained ...

  • Garmin G1000H - page 274

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 262 FLIGHT MANA GEMENT 7) As the CDI approaches center , the aircraft turns onto the active leg as seen in Figure 5-116. Figure 5-116 T urn on to Active Leg 8) At SLN , Victor Airw ay 244 (V244) is intercepted. T urn prompts are displayed in the PFD Navigation Status Box as ...

  • Garmin G1000H - page 275

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 263 FLIGHT MANA GEMENT 9) As seen in Figure 5-118, V244 is now the active flight plan leg. Figure 5-118 V244 Now Active Leg ...

  • Garmin G1000H - page 276

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 264 FLIGHT MANA GEMENT 10) At Lamar VOR (LAA) V263 is intercepted. See Figure 5-119. Figure 5-119 HY S to LAA Leg Active 11) A TC grants clear ance to proceed direct to the OPSHN intersection to begin the arrival procedure . A TC advises to expect an altitude of 10,000 feet ...

  • Garmin G1000H - page 277

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 265 FLIGHT MANA GEMENT d) T urn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 5-121. Figure 5-121 Enter VNV Altitude e) An altitude of 10,000 feet is entered as requested by A TC . f) Press the ENT K ey . T he cursor is now displayed in ...

  • Garmin G1000H - page 278

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 266 FLIGHT MANA GEMENT h) Press the ENT K ey twice to activate the direct-to . Note , in Figure 5-123, the magenta arrow indicating the direct-to OPSHN after the offset waypoint for OPSHN . T he preceding offset waypoint indicates the offset distance and altitude that were p ...

  • Garmin G1000H - page 279

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 267 FLIGHT MANA GEMENT b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 5-124. Figure 5-124 Procedur es Window c) Press the ENT K ey . A list of available approaches for the destination airport is displayed as in Figure 5-125. Figure 5-125 List of Available ...

  • Garmin G1000H - page 280

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 268 FLIGHT MANA GEMENT e) Press the ENT K ey . A list of av ailable transitions for the selected approach is displayed as in Figure 5-126. Figure 5-126 List of Available T ransitions f) T urn either FMS Knob to select the desired tr ansition. In this case , the Initial Appro ...

  • Garmin G1000H - page 281

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 269 FLIGHT MANA GEMENT Figure 5-127 Barometric Minimums Set i) With ‘LOAD?’ highlighted, again press the ENT K ey . T he selected approach is added to the flight plan as seen in Figure 5-128. Figure 5-128 Loaded Approach ...

  • Garmin G1000H - page 282

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 270 FLIGHT MANA GEMENT 13) Note the altitude constr aints associated with each of the approach waypoints as seen in Figure 5-129. T hese altitudes are loaded from the database and are displayed as light blue text, indicating these values are “designated” for use in compu ...

  • Garmin G1000H - page 283

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 271 FLIGHT MANA GEMENT 14) As the aircr aft approaches OPSHN, it may be desirable to adjust the speed, or steepness of the upcoming descent. T he default Flight P ath Angle (FP A) is -3.0 degrees and a required vertical speed is computed to maintain the -3.0 FP A. T o change ...

  • Garmin G1000H - page 284

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 272 FLIGHT MANA GEMENT 15) As seen in Figure 5-131, the aircraft is approaching T OD . Note the target vertical speed required to reach the selected altitude . T he V ertical Deviation Indicator (VDI) and the Required V ertical Speed Indicator (RVSI) are now displayed on the ...

  • Garmin G1000H - page 285

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 273 FLIGHT MANA GEMENT 16) Upon reaching T OD , a descent vertical speed is established by placing the VSI pointer in line with the RVSI as shown in Figure 5-133. Figure 5-133 VDI & RVSI Showing Correctly Established Descent Align Actual V ertical Speed with Required V e ...

  • Garmin G1000H - page 286

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 274 FLIGHT MANA GEMENT 18) T he aircraft is approaching OPSHN . T he upcoming turn and next heading are annunciated at the top left of the PFD as seen in Figure 5-135. Initiate the turn and maneuver the aircraft on a tr ack through the turn radius to intercept the magenta li ...

  • Garmin G1000H - page 287

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 275 FLIGHT MANA GEMENT 19) After passing OPSHN, the next leg of the arrival turns magenta as shown in Figure 5-136. T he magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active . Figure 5-136 T racking the OPSHN to F ...

  • Garmin G1000H - page 288

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 276 FLIGHT MANA GEMENT Figure 5-137 Approaching PYNON ...

  • Garmin G1000H - page 289

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 277 FLIGHT MANA GEMENT 21) Upon passing PYNON the approach procedure automatically becomes active . T he approach may be activated at any point to proceed directly to the IAF . In this example , the aircraft has progressed through the final waypoint of the arriv al and the ...

  • Garmin G1000H - page 290

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 278 FLIGHT MANA GEMENT 22) T he IAF is the next waypoint. At the T OD , establish a descent vertical speed as previously discussed in Step 16. T he aircraft altitude is 9,000 feet upon reaching HABUK. Figure 5-140 Descending T urn to the Initial Approach Fix (IAF) ...

  • Garmin G1000H - page 291

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 279 FLIGHT MANA GEMENT 23) After crossing F ALUR the next waypoint is the F AF . The flight phase changes to LPV on the HSI indicating the current phase of flight is in Approach Mode and the approach type is LPV . CDI scaling changes accordingly and is used much lik e a lo ...

  • Garmin G1000H - page 292

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 280 FLIGHT MANA GEMENT 24) After crossing CEGIX, the aircr aft continues following the glidepath to maintain the descent to “ A T or ABOVE” 6,370 feet at the Missed Approach P oint (MAP) (RW35R) as seen in Figure 5-142. Figure 5-142 Descending to the Missed Approach P oi ...

  • Garmin G1000H - page 293

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 281 FLIGHT MANA GEMENT 25) Upon reaching the MAP , it is decided to execute a missed approach. Automatic waypoint sequencing is suspended past the MAP . Press the Go Around Button, or press the SUSP Softk ey on the PFD , to resume automatic waypoint sequencing through the mi ...

  • Garmin G1000H - page 294

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 282 FLIGHT MANA GEMENT 26) T he aircraft continues climbing to “ A T or ABOVE” 10,000 feet at MOGAL. A holding pattern is established at the MAHP (MOGAL) as shown in Figure 5-144. Figure 5-144 Establishing the Holding P attern 27) T he aircraft maintains 10,000 feet whil ...

  • Garmin G1000H - page 295

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 283 FLIGHT MANA GEMENT 5.12 ABNORMAL OPERA TION ThissectiondiscussestheDeadReckoningmodeofoperationandthesubsequentindications. NO TE: Dead Reck oning Mode only functions in Enroute (ENR) or Oceanic (OCN) phase of flight. In all other pha ...

  • Garmin G1000H - page 296

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 284 FLIGHT MANA GEMENT Distance & Bearing GPS Navigation Lost Message Dead Reckoning Annunciaion Figure 5-146 Dead Reckoning Mode - GPS Derived Data Shown in Y ellow Dead Reckoning Annunciation Subdued Rotorcraft Symbol Nav Data Bar All data except Active Leg, T AS, and ...

  • Garmin G1000H - page 297

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 285 HAZARD A VOID ANCE SECTION 6 HAZARD A VOID ANCE The G1000H hazard avoidance featur es are designed to provide advisory information of potential hazar ds to flight safety associated with weather , terrain, and air traffic. This section is divided into the following grou ...

  • Garmin G1000H - page 298

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 286 HAZARD A VOID ANCE SiriusXMusesthecodedIDsto sendanactivationsignalthatallowsthesystemto displayweatherdataand/ orentertainmentprogrammingpr ovidedthroughtheGDL69AH. Activating XM WX Satellite W e ...

  • Garmin G1000H - page 299

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 287 HAZARD A VOID ANCE 4) Press the MENU Ke y. 5) T urn the FMS Knob to highlight ‘Display XM Weather’ and press the ENT K ey . P age title displays ‘MAP - WEA THER DA T A LINK (XM)’ to indicate XM WX is the selected weather datalink source . Figure 6-2 W eather Data ...

  • Garmin G1000H - page 300

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 288 HAZARD A VOID ANCE W eather Product Symbol Expiration Time (Minutes) Refresh Rate (Minutes) Next-generation Radar (NEXRAD) 30 5 (U .S .) 10 (Canada) Cloud T op (CLD T OP) 60 15 Echo T op (ECHO T OP) 30 7.5 XM Lightning (L TNG) 30 5 Cell Movement (CELL MOV) 30 12 SIGMETs/ ...

  • Garmin G1000H - page 301

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 289 HAZARD A VOID ANCE T able6-2showswhichXMWXproductscanbedisplayed(indicatedwitha‘+’symbol)onspecicmaps. W eather Product PFD Inset Map Navigation Map P age W eather Data Link (XM) P age W eather Information P age A ...

  • Garmin G1000H - page 302

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 290 HAZARD A VOID ANCE Softkeyscontrolthedisplay ofweatherinformation onmostMFD pagesandthe PFDInsetMap (Figure6-3 shows the weather pr oduct softkeys for the W eatherData Link (XM)Page).? ...

  • Garmin G1000H - page 303

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 291 HAZARD A VOID ANCE Setting up and customizing the W eather Data Link (XM) P age: 1) Select the Weather Data Link (XM) P age . 2) Press the MENU Ke y. 3) With ‘Weather Setup’ highlighted, press the ENT K ey (Figure 6-4). 4) T urn the small FMS Knob to select ‘Produc ...

  • Garmin G1000H - page 304

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 292 HAZARD A VOID ANCE Mapsbesides theW eather DataLink(XM) Pageuse settingsbasedon thoseselectedfor theNavigation Map Page. Setting up and customizing weather data for the Navigation Map P age: 1) Select the Navigatio ...

  • Garmin G1000H - page 305

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 293 HAZARD A VOID ANCE Viewing legends for displayed weather pr oducts: 1) Select the Weather Data Link (XM) P age . 2) Select the LEGEND Softk ey to display the legends for the displayed weather products . Or : a) Press the MENU Ke y. b) Select ‘Weather Legend’ and pres ...

  • Garmin G1000H - page 306

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 294 HAZARD A VOID ANCE NEXRAD NOTE: NEXRAD data cannot be displayed at the same time as turbulence, icing, or terrain. WSR-88D, or NEXRAD (NEXt-generation RADar), is a network of 158 high-resolution Doppler radar systems that are? ...

  • Garmin G1000H - page 307

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 295 HAZARD A VOID ANCE Displaying NEXRAD weather information: 1) Select the MAP Softk ey (for the PFD Inset Map , select the INSET Softk ey). T his step is not necessary on the Weather Data Link (XM) P age . 2) Select the NEXRAD Softk ey . Compositedata fr omall ...

  • Garmin G1000H - page 308

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 296 HAZARD A VOID ANCE neXRaD l imit a tiOns NEXRADradarimagesmayhavecertainlimitations: • NEXRAD base reectivity does not provide sufcient information to determine cloud layers or precipitation character ...

  • Garmin G1000H - page 309

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 297 HAZARD A VOID ANCE neXRaD l imit a tiOns (c anaD a ) • Radarcoverageextendsto55ºN. • Anyprecipitationdisplayedbetween52ºNand55ºNisdisplayedasmixedbecauseitisunknown. Figure 6-13 NEXRAD Data - Canada No Co ...

  • Garmin G1000H - page 310

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 298 HAZARD A VOID ANCE ECHO T OPS NOTE: Display of Echo T ops cannot be displayed at the same time as Cloud T ops and NEXRAD . Echo T ops data (Figure6-14) shows the location, elevation, and direction ofthe highest radar echo. ...

  • Garmin G1000H - page 311

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 299 HAZARD A VOID ANCE The display of radar coverage is always active when either NEXRAD or ECHO TOPS is selected.  Areas where NEXRADradar coverageand EchoT opsinformation isnot currently ...

  • Garmin G1000H - page 312

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 300 HAZARD A VOID ANCE XM LIGHTNING Lightning data (Figure 6-18) showsthe approximate location of cloud-to-ground lightning strikes. Astrike iconrepresentsastrikethathas occurredwithinatwo-kilometerre ...

  • Garmin G1000H - page 313

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 301 HAZARD A VOID ANCE CELL MO VEMENT Cell Movement data (Figure 6-20) shows the location and movement of storm cells as identied by the ground-based system.  Cells are repr esented by yellow squar ...

  • Garmin G1000H - page 314

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 302 HAZARD A VOID ANCE SIGMETS AND AIRMETS SIGMET  (SIGnicantMET eor ological Information) and AIRMET (AIRmen’ s MET eorologicalInformation) are issued for potentially hazar dous weather .  A Convective SIGMET is? ...

  • Garmin G1000H - page 315

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 303 HAZARD A VOID ANCE MET ARS AND T AFS NOTE: Atmospheric pressure as reported for MET ARs is given in hectopascals (hP a), except for in the United States , where it is reported in inches of mercury (in Hg). T emperatures are reported in Celsius . NOTE: MET AR information ...

  • Garmin G1000H - page 316

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 304 HAZARD A VOID ANCE 4) T urn the FMS Knob or the ENT K ey to scroll through the MET AR and T AF text. MET AR text must be completely scrolled through before scrolling through the T AF text. 5) Press the FMS Knob or the CLR K ey to return to the Weather Data Link (XM) P ag ...

  • Garmin G1000H - page 317

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 305 HAZARD A VOID ANCE Displaying raw MET AR text on the Active Flight Plan P age: 1) Select the Active Flight Plan P age on the MFD . 2) Press the FMS Knob to activate the cursor . 3) T urn the large FMS Knob to highlight a w aypoint with an associated MET AR. T he MET AR t ...

  • Garmin G1000H - page 318

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 306 HAZARD A VOID ANCE SURF ACE ANAL Y SIS AND CITY FORECAST NOTE: Surface Analysis and City Forecast data are displayed only within the installed navigation database service area. Surface Analysis and City Forecast information is available for cur ...

  • Garmin G1000H - page 319

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 307 HAZARD A VOID ANCE FREEZING LEVELS Freezing Level data shows the color -coded contour lines for the altitude and location at which the rst isothermis found(Figur e6-30). When nodata isdis ...

  • Garmin G1000H - page 320

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 308 HAZARD A VOID ANCE WINDS ALOFT W inds Aloft data (Figure 6-32) shows the forecasted wind speed and direction at the surface and at selected altitudes.Altitudecanbedisplayedin3,000-footincrements? ...

  • Garmin G1000H - page 321

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 309 HAZARD A VOID ANCE COUNTY W ARNINGS County data (Figure 6-34) provides specic public awareness and protection weather warnings from the National W eather Ser vice (NWS).  This can include information on ...

  • Garmin G1000H - page 322

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 310 HAZARD A VOID ANCE CYCLONE The Cyclone weather product (Figure 6-36) shows the current location of cyclones (hurricanes), tropical storms,andtheirprojectedtracks. Figure 6-36 Cyclone Data Selected for Display Cyclone ...

  • Garmin G1000H - page 323

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 311 HAZARD A VOID ANCE ICING (CIP & SLD) NOTE: Icing data cannot be displayed at the same time as NEXRAD data. Current Icing Product (CIP) data shows a graphical view of the current icing environment (Figure 6-38).  Icin ...

  • Garmin G1000H - page 324

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 312 HAZARD A VOID ANCE TURBULENCE NOTE: T urbulence data cannot be displayed at the same time as NEXRAD data. T urbulence data (Figure 6-40) identies the potential for erratic movement of high-altitude air mass associatedwinds. ...

  • Garmin G1000H - page 325

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 313 HAZARD A VOID ANCE PIREPS AND AIREPS Pilot W eather Reports (PIREPs) describein-ight weatherencounter edby pilots.  When signicantweather conditions are reportedor forecast, Air T rafcContr ol(A T ...

  • Garmin G1000H - page 326

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 314 HAZARD A VOID ANCE Figure 6-43 PIREP T ext on the W eather Data Link (XM) P age Decoded PIREP T ext Raw PIREP T ext Selected PIREP Age of report in HH:MM T o display thePIREP or AIREP legend (Figure 6-44),press the LEGEND Softkey wh ...

  • Garmin G1000H - page 327

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 315 HAZARD A VOID ANCE 6.2 GFDS WORLDWIDE WEA THER NOTE: Garmin Flight Data Services Worldwide Weather provides information for avoiding hazardous weather . Do not utilize Worldwide Weather information to penetrate hazardous weather . NOTE: T he availability of specific GFD ...

  • Garmin G1000H - page 328

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 316 HAZARD A VOID ANCE Figure 6-45 GFDS W eather Data Link (GFDS) P age (After GFDS W eather Request) Weather product age information Precip Weather Product Display Enabled icon Precip Weather Product Selected for Display When a weather product is selected ...

  • Garmin G1000H - page 329

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 317 HAZARD A VOID ANCE W eather Product Symbol Expiration Time (Minutes) Refresh Rate (Minutes) Radar Precipitation (PRECIP) 30 U. S. : 3 * Canada: 3* † Europe: 15 Australia: 15ˆ Infrared Satellite (IR SA T) 60 30 Datalink Lightning (DL L TNG) 30 Continuous SIGMETs/AIRMET ...

  • Garmin G1000H - page 330

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 318 HAZARD A VOID ANCE T able 6-4 shows which GFDS W eather products can be displayed (indicated with a ‘+’ symbol) on specic G1000H maps. GFDS W eather Product PFD Inset Map Navigation Map P age W eather Data Link (G ...

  • Garmin G1000H - page 331

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 319 HAZARD A VOID ANCE Figure 6-46 GFDS W eather Product Softkeys (MFD) Press the BACK Softkey to move up one level. BAC K PRECIP MORE WX DL LT NG IR SA T SIG/AIR MET AR LEGEND CHKLIST 9000 1 2000 6 000 BAC K LEGEND 3000 15000 SFC PREV OFF NEXT 27000 3 0000 2 400 0 BAC K LEG ...

  • Garmin G1000H - page 332

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 320 HAZARD A VOID ANCE Figure 6-48 W eather Data Link (GFDS) P age Setup Menu Figure 6-47 W eather Data Link (GFDS) P age Menu Restoring default W eather Data Link (GFDS) P age settings: 1) Select the Weather Data Link (GFDS) P age . 2) Press the MENU Ke y. 3) With ‘Weathe ...

  • Garmin G1000H - page 333

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 321 HAZARD A VOID ANCE If both GFDSand XM weather services areinstalled, customizing the display settingsfor the corresponding weatherproductsshowninT able6-5willresultinidenticalsettingsforb ...

  • Garmin G1000H - page 334

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 322 HAZARD A VOID ANCE Figure 6-50 Navigation Map P age Setup Menu Figure 6-49 Navigation Map P age Menu Figure 6-51 Navigation Map P age Setup Menu, W eather Group Each active weather pr oduct has an associated legend which can be displayed? ...

  • Garmin G1000H - page 335

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 323 HAZARD A VOID ANCE Figure 6-52 P anning on the GFDS Data Link P age Additional In- formation on TFR Selected with Map Pointer TFR Selected with Map Pointer GFDS WEA THER D A T A REQUESTS The GFDS Data Request window pr ovides the ight crew w ...

  • Garmin G1000H - page 336

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 324 HAZARD A VOID ANCE  • DESTINA TION – Requests data based on the active flight plan destination (Direct-T o destinations excluded). See the Flight Management section for more information about entering and activating flight plans .  • FPL – Requests ...

  • Garmin G1000H - page 337

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 325 HAZARD A VOID ANCE Figure 6-55 GFDS W eather Data Request Results with Precipitation and Infrared Satellite Displayed Present Position Selected, 200 nm Diameter Requested Destination Selected, 200 nm Diameter Requested Next 80 nm of Flight Plan Selected, 200 nm Route Wid ...

  • Garmin G1000H - page 338

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 326 HAZARD A VOID ANCE Atthecompletionofasuccessfulweatherdatarequest,therequeststatuswindow(ifstillopen)willindicate ‘OK’. Cancelling a GFDS W eather Data Request in Progress: 1) Select the Weather Data Link (GFDS) P ...

  • Garmin G1000H - page 339

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 327 HAZARD A VOID ANCE WORLDWIDE WEA THER PRODUCTS PRECIPIT A TION Precipitation (PRECIP) data is not real-time.  The lapsed time between collection, pr ocessing, and dissemination ofradar images canbe signicant? ...

  • Garmin G1000H - page 340

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 328 HAZARD A VOID ANCE No Radar Coverage Figure 6-57 Precipitation Data Legend Boundary of GFDS weather data request The display of radar coverage is enabled when Precipitation is selected for display .  Areas where precipitati ...

  • Garmin G1000H - page 341

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 329 HAZARD A VOID ANCE Figure 6-58 Precipitation Data - Zoomed Block represents 4 km 2 Thefollowingmaycauseabnormalitiesindisplayedradarimages: • Groundclutter • Strobesandspuriousradardata • Sunstrobes(whenthe? ...

  • Garmin G1000H - page 342

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 330 HAZARD A VOID ANCE INFRARED SA TELLITE Infrared Satellite (IR SA T) data (Figure 6-59) depicts cloud top temperatures from satellite imagery .  Brighter cloud top colors indicate cooler temperatures occurring at higher alti ...

  • Garmin G1000H - page 343

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 331 HAZARD A VOID ANCE D A T ALINK LIGHTNING Datalink Lightning (DL L TNG) data (Figure 6-61) shows the appr oximate location of cloud-to-ground lightningstrikes. A strikeicon repr esents astrike thathas ...

  • Garmin G1000H - page 344

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 332 HAZARD A VOID ANCE SIGMETS AND AIRMETS SIGMET s  (SIGnicant MET eorological Information) and AIRMET s (AIRmen’ s MET eor ologicalInformation) are issued for potentially hazar dous weather .  A Convective SIGMET? ...

  • Garmin G1000H - page 345

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 333 HAZARD A VOID ANCE MET ARS AND T AFS NOTE: MET AR information is only displayed within the installed navigation database service area. MET ARs (MET eor ological Aerodr ome Reports) typically contain information about the temperature, dewpoin ...

  • Garmin G1000H - page 346

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 334 HAZARD A VOID ANCE 1) Select the Weather Information P age . a) T urn the large FMS Knob to select the W aypoint P age Group . b) Select the WX Softk ey to select the Weather Information P age . 2) Press the FMS Knob to display the cursor . 3) Use the FMS Knob to enter t ...

  • Garmin G1000H - page 347

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 335 HAZARD A VOID ANCE The MET AR ag color is determined by the information in the MET AR text.  A gray MET AR ag is displayed whentheMET ARtextdoesnotcontainadequateinformation. Figure ...

  • Garmin G1000H - page 348

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 336 HAZARD A VOID ANCE PIREPS Pilot W eather Reports (PIREPs) describe in-ight weather encountered by pilots.  A PIREP may contain adverse weatherconditions, suchas low in-ightvisibility ,icing con ...

  • Garmin G1000H - page 349

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 337 HAZARD A VOID ANCE Figure 6-72 PIREP T ext on the W eather Data Link (GFDS) P age Decoded PIREP T ext Raw PIREP T ext T o display the PIREP or AIREP legend (Figure 6-73) , select the LEGEND  Softkey when PIREPs or AIREPs  are ...

  • Garmin G1000H - page 350

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 338 HAZARD A VOID ANCE ABNORMAL OPERA TIONS If the G1000H cannot complete a GFDS weather data request, one or more messages will appear in the requeststatuswindow . W eather Request Status Message Desciption Auto re ...

  • Garmin G1000H - page 351

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 339 HAZARD A VOID ANCE TheG1000H alsodisplaysmessageadvisories onthePFD whichmayindicate apr oblemwiththe GDL59H; refertoAppendixAformoreinformation. GFDS WEA THER IN REVERSIONAR Y MODE When the G1 ...

  • Garmin G1000H - page 352

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 340 HAZARD A VOID ANCE 6.3 HT AWS WARNING: Do not use HT AWS information for primary terrain avoidance . HT AWS is intended only to enhance situational awareness . NOTE: T he data contained in the HT AWS databases comes from government agencies . Garmin accurately processes ...

  • Garmin G1000H - page 353

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 341 HAZARD A VOID ANCE from the altimeter) to dif fer from the GSL altitude.  This variation results in the aircraft’ s GSL altitude differing fromthebar o-correctedaltitude. DISPLA YING HT AWS D A T A HT A ...

  • Garmin G1000H - page 354

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 342 HAZARD A VOID ANCE HT A WS P A GE The MAP- HT A WS Pageis specialized toshow terrain,obstacle, and potentialimpact point datain relation totheair craft’ scurrentaltitude,withoutclutterfr omth ...

  • Garmin G1000H - page 355

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 343 HAZARD A VOID ANCE Figure 6-75 HT A WS P age (360 View) T errain Legend Map Range Rings Obstacles Annunciation Window Current Aircraft GPS- derived GSL Altitude Map Orientation Figure 6-76 HT A WS P age (ARC View) T errain Legend Map Range Arc Annunciation Window Current ...

  • Garmin G1000H - page 356

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 344 HAZARD A VOID ANCE HT A WS ALERTS Alerts are issued when ight conditions meet parameters that are set within HT A WS software algorithms.  HT A WS alerts typically employ a CAUTION or a W ARNING? ...

  • Garmin G1000H - page 357

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 345 HAZARD A VOID ANCE Alert T ype PFD/HT A WS P age Alert Annunciation MFD P op-Up Alert (except HT A WS P age) Aural Message Reduced Required T errain Clear ance W arn ing (R TC) “W arning; T errain, T errain” Imminent T errain Impact W arning (ITI) “W arning; T erra ...

  • Garmin G1000H - page 358

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 346 HAZARD A VOID ANCE Imminent T errain Impact (ITI) and Imminent Obstacle Impact (IOI) alerts are issued when the aircraft is below the elevation of a terrain or obstacle cell in the air craft’ s projected path.  ITI ...

  • Garmin G1000H - page 359

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 347 HAZARD A VOID ANCE Enabling/Disabling RP Mode: 1) T urn the large FMS Knob to select the HT AWS P age . 2) Press the RP MODE Softk ey to inhibit or enable RP Mode (choice dependent on current state). Or : 1) Press the MENU Ke y. 2) T urn the FMS Knob to select ‘Reduce ...

  • Garmin G1000H - page 360

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 348 HAZARD A VOID ANCE AL TITUDE VOICE CALLOUT (VCO) AURAL ALER TS HT A WS provides aural altitude advisory alerts as the aircraft descends.  VCO alerts are based on either radar altitude(ifaradaraltimeteri ...

  • Garmin G1000H - page 361

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 349 HAZARD A VOID ANCE SY STEM ST A TUS During systempower -up, HT A WS conducts asystem-test of itsaural and visual annunciations. The system test can also be manually initiated.  An aural alert i ...

  • Garmin G1000H - page 362

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 350 HAZARD A VOID ANCE ‘HT A WSN/A ’isgeneratedintheannunciationwindowand ontheHT A WSPage.Theauralmessage “HT A WS Not A vailable” isalso generated.When sufcientGPSsignal isreceived? ...

  • Garmin G1000H - page 363

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 351 HAZARD A VOID ANCE 6.4 TRAFFIC INFORMA TION SERVICE (TIS) W ARNING : T he T raffic Information Service (TIS) is intended for advisory use only . TIS is intended to help the pilot locate traffic visually . It is the responsibility of the pilot to see and maneuver to avo ...

  • Garmin G1000H - page 364

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 352 HAZARD A VOID ANCE DISPLA YING TRAFFIC DA T A T rafcinformationcanbedisplayedonthefollowingmaps(whenTISisoperating): • PFDInsetMap • NavigationMapPage • T rafcMapPage • T ripPlanningPag ...

  • Garmin G1000H - page 365

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 353 HAZARD A VOID ANCE Customizing traffic display on the Navigation Map P age: 1) Select the Navigation Map P age . 2) Press the MENU Ke y. 3) With ‘Map Setup’ highlighted, press the ENT K ey (Figure 6-85). 4) T urn the small FMS Knob to select the ‘T raffic’ Grou ...

  • Garmin G1000H - page 366

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 354 HAZARD A VOID ANCE The Navigation Map Page Setup Menu provides a means in addition to the softkey for enabling/disabling display of trafc.  The setup menu also controls the map range s ...

  • Garmin G1000H - page 367

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 355 HAZARD A VOID ANCE TIS ALERTS WhenthenumberofT AsontheT rafcMapPageincreasesfromonescantothenext,thefollowingoccur: • Asingle “T raffic” voice alert is generated. • A ‘TRAFFIC’ Ann ...

  • Garmin G1000H - page 368

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 356 HAZARD A VOID ANCE Or : a) Press the MENU Ke y. b) Select ‘ ‘’Not Available” Mute On’ (shown if TNA muting is currently off) and press the ENT Ke y. SY STEM ST A TUS TheG1000H performs anautomatic testof TISduring power -up. If? ...

  • Garmin G1000H - page 369

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 357 HAZARD A VOID ANCE Mode T raffic Mode Annunciation (T raffic Map P age) T raffic Display Enabled Icon (Other Maps) TIS Operating OPERA TING TIS Standby ST ANDBY (also shown in white in center of page) TIS F ailed* F AIL * See T able 6-15 for additional failure annunci ...

  • Garmin G1000H - page 370

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 358 HAZARD A VOID ANCE 6.5 GARMIN GTS TRAFFIC WARNING: T he Garmin GTS 800 T raffic Advisory System (T AS) is intended for advisory use only to aid the pilot in visually acquiring traffic. No avoidance maneuvers should be based solely upon T AS traffic information. It is ...

  • Garmin G1000H - page 371

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 359 HAZARD A VOID ANCE When paired with a 1090 MHz extended squitter transponder , the GTS 800 uses Automatic Dependent Surveillance - Broadcast (ADS-B) data fr om participating airbor ne air craft trans ...

  • Garmin G1000H - page 372

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 360 HAZARD A VOID ANCE A vertical trend arrow to the right of the intruder symbol (Figure 6-91) indicates climbing or descending trafcwithanupwardordownwar d-pointingarrowr espectively . Relative A ...

  • Garmin G1000H - page 373

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 361 HAZARD A VOID ANCE Sensitivity Level Intruder Altitude A vailable T A Alerting Conditions A Ye s Intruder closing rate provides less than 20 seconds of vertical and horizontal separation. Or: Intruder closing rate provides less than 20 seconds of horizontal separation an ...

  • Garmin G1000H - page 374

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 362 HAZARD A VOID ANCE AT Awillbedisplayed foratleasteightseconds, evenifthe condition(s)thatinitially triggeredthe T Aareno longer present. Figure 6-93 T raffic Annunciation (PFD) Inset Map Displays When T A is ...

  • Garmin G1000H - page 375

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 363 HAZARD A VOID ANCE 3) T urn the Range knob to set the r ange to 2/6 nm to allow for the full test pattern to be displayed. 4) Select the TEST Softk ey . Or: 1) Press the MENU K ey and turn the small FMS knob to select ‘T est Mode’. 2) Press the ENT Ke y. T A at 9 o? ...

  • Garmin G1000H - page 376

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 364 HAZARD A VOID ANCE Switching from standby mode to operating mode: O n the T raffic P age , select the OPERA TE Softk ey Or: 1) Press the MENU K ey and turn the small FMS knob to select ‘Operate Mode’. 2) Press the ENT K ey . T he system switches from Standby Mode to ...

  • Garmin G1000H - page 377

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 365 HAZARD A VOID ANCE a l titUDe D isPla y The pilot can select the volume of airspace in which non-threat and pr oximity trafc is displayed.  T As occurringoutsideoftheselimitswillalwaysbeshow ...

  • Garmin G1000H - page 378

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 366 HAZARD A VOID ANCE F light iD D isPla y The Flight IDs of other aircraft (when available) can be enabled for display on the T rafc Map Page (Figure 6-96).When aightID isreceived, it ...

  • Garmin G1000H - page 379

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 367 HAZARD A VOID ANCE Enabling/Disabling Flight ID Display: On the T raffic Map P age , select the FL T ID Softk ey . Or : 1) Press the MENU Ke y. 2) T urn the small FMS Knob to select ‘Show Flight IDs’ or ‘Hide Flight IDs’ (choice dependent on current state) (Figu ...

  • Garmin G1000H - page 380

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 368 HAZARD A VOID ANCE ADDITIONAL TRAFFIC DISPLA Y S T rafcinformationcanbedisplayedonthefollowingmapsontheMFDwhentheunitisoperating: • NavigationMapPage • T rafcMapPage • T ripPlanningPag ...

  • Garmin G1000H - page 381

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 369 HAZARD A VOID ANCE Customizing the traffic display on the Navigation Map P age: 1) Select the Navigation Map P age . 2) Press the MENU Ke y. 3) With Map Setup highlighted, press the ENT K ey (Figure 6-99). 4) T urn the small FMS Knob to select the T raffic Group and pr ...

  • Garmin G1000H - page 382

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 370 HAZARD A VOID ANCE The Navigation Map Page SetupMenu also controls the display of trafc.  The setup menu controls the map range settings. T rafc data symbolsand labels can bedecl ...

  • Garmin G1000H - page 383

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 371 HAZARD A VOID ANCE Theannunciations toindicatethe statusof trafcinformation appearina bannerat thelower leftcornerof mapsonwhichtrafccanbedisplayed. T raffic Status Banner Annunciation Desc ...

  • Garmin G1000H - page 384

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 372 HAZARD A VOID ANCE B lank P age ...

  • Garmin G1000H - page 385

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 373 A UTOMA TIC FLIGHT CONTROL SYSTEM SECTION 7 A UT OMA TIC FLIGHT CONTROL SY STEM Not available. ...

  • Garmin G1000H - page 386

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 374 A UTOMA TIC FLIGHT CONTROL SYSTEM B lank P age ...

  • Garmin G1000H - page 387

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 375 ADDITIONAL FEA TURES SECTION 8 ADDITIONAL FEA TURES NOTE: With the availability of SafeT axi, ChartView , or FliteCharts in electronic form, it is still advisable to carry another source of charts on board the aircraft. Additional features of the system include the follo ...

  • Garmin G1000H - page 388

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 376 ADDITIONAL FEA TURES 8.1 SYNTHETIC VISION SYSTEM (SVS) W ARNING: 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 either the accuracy or reliab ...

  • Garmin G1000H - page 389

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 377 ADDITIONAL FEA TURES Figure 8-1 Synthetic Vision Imagery SVS OPERA TION SVS isactivated fromthe PFD usingthe softkeys locatedalong the bottom edgeof the display .  Pr essing the softkeys turns therelate ...

  • Garmin G1000H - page 390

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 378 ADDITIONAL FEA TURES Figure 8-2 SVS Softkeys Pressing the BACK Softkey returns to the top-level softkeys. BA CK BA CK PFD Pressing the BACK Softkey returns to the previous level of softkeys. SYN VIS PA TH WA YS YN TERR HRZN HDG APTSIGNS Activating and deactivating SVS: 1 ...

  • Garmin G1000H - page 391

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 379 ADDITIONAL FEA TURES SVS FEA TURES Figure 8-3 SVS on the Primary Flight Display SVS Softkeys Synthetic T errain Pathways Flight Path Marker Airport Runway Zero Pitch Line (ZPL) with Compass Heading Marks Airplane Symbol Selected Altitude NOTE: P athways and terrain featu ...

  • Garmin G1000H - page 392

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 380 ADDITIONAL FEA TURES Figure 8-4 Progr ammed and Selected Altitude Selected Altitude Programmed Altitudes Pathways pr ovide supplemental glidepath/glideslope information on anactive ILS, LPV , LNA V/VNA V , and some LNA V appr oac ...

  • Garmin G1000H - page 393

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 381 ADDITIONAL FEA TURES D escent anD a PPROa ch Pathways are showndescending only fora pr ogrammed descent(Figur es8-5, 8-6). When the ightplan includesprogrammeddescent segments,pathways aredisplayed? ...

  • Garmin G1000H - page 394

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 382 ADDITIONAL FEA TURES m isseD a PPROa ch Upon activatingthe missed approach, pathways leadto the MissedAppr oach Holding Point(MAHP) and aredisplayed as a level path atthe published altitude for ...

  • Garmin G1000H - page 395

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 383 ADDITIONAL FEA TURES FLIGHT P A TH MARKER NOTE: T he Flight P ath Mark er is not available when the cross-pointer (X-P ointer) flight director format is selected. The Flight PathMarker (FPM), also known as a V elocity V ector , is dis ...

  • Garmin G1000H - page 396

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 384 ADDITIONAL FEA TURES HORIZON HEADING The Horizon Heading is synchronized with the HSI and shows appr oximately 60 degrees of compass heading in 30-degree incr ements on the ZeroPitch Line.  Horizo ...

  • Garmin G1000H - page 397

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 385 ADDITIONAL FEA TURES RUNW A Y S W ARNING: 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. NOTE: Not all airports have runways with endpoint dat ...

  • Garmin G1000H - page 398

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 386 ADDITIONAL FEA TURES HT AWS ALER TING T errainalertingonthesyntheticterrain displayistriggered byForward-looking T errainA voidance(FL T A).  When an obstacle becomes a potential impact point the col ...

  • Garmin G1000H - page 399

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 387 ADDITIONAL FEA TURES Obstacles are represented on the synthetic terrain display by standard two-dimensional tower symbols as foundonMFDHT A WSPageandcharts. Obstaclesymbolsappearintheperspec ...

  • Garmin G1000H - page 400

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 388 ADDITIONAL FEA TURES FIELD OF VIEW The PFD eld of view can be represented on the MFD Navigation Map Page.  T wo dashed lines forming a V -shapeinfr ontoftheaircraftsymbolonthemap,? ...

  • Garmin G1000H - page 401

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 389 ADDITIONAL FEA TURES The following gure compares the PFD forward looking depiction with the MFD plan view and FIELD OF VIEWturnedon. Figure 8-13 PFD and MFD Field of View Comparison Lines Depict PFD Field of Vie ...

  • Garmin G1000H - page 402

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 390 ADDITIONAL FEA TURES 8.2 SAFET AXI SafeT axi is an optional feature that gives greater map detail when viewing airports at close range.  The maximum maprangesfor enhanceddetailare pilotcongu ...

  • Garmin G1000H - page 403

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 391 ADDITIONAL FEA TURES Figure 8-14 SafeT axi Depiction on the Navigation Map P age DCL TR Softkey Removes T axiway Markings Airport Features Aircraft Position T axiway Identification Airport Hot Spot Outline The DCL TR  Softkey(declutter)labeladvancesto ...

  • Garmin G1000H - page 404

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 392 ADDITIONAL FEA TURES Configuring SafeT axi range: 1) While viewing the Navigation Map P age , press the MENU K ey to display the P AGE MENU . 2) T urn the large FMS Knob to highlight the Map Setup Menu Option and press the ENT Ke y. Figure 8-15 Navigation Map P A GE MEN ...

  • Garmin G1000H - page 405

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 393 ADDITIONAL FEA TURES SafeT axi database is revised every 56 days.  SafeT axi is always available for use after the expiration date.  When tur ning on the system, the Power -up Page indicates ...

  • Garmin G1000H - page 406

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 394 ADDITIONAL FEA TURES TheSafeT axidatabasecyclenumbershowninthegure,10S5,isdecipheredasfollows: 10–Indicatestheyear2010 S–IndicatesthedataisforSafeT axi 5–Indicatesthefth ...

  • Garmin G1000H - page 407

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 395 ADDITIONAL FEA TURES Figure 8-19 illustrates possible SafeT axi database conditions that may appear on the  AUX-System Status Page.  The EFFECTIVE date is the beginning date for this data ...

  • Garmin G1000H - page 408

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 396 ADDITIONAL FEA TURES 8.3 CHARTVIEW ChartView is an optional feature resembling the paper version of Jeppesen terminal procedures charts.  The charts are displayed in full color with high-resolution. ...

  • Garmin G1000H - page 409

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 397 ADDITIONAL FEA TURES TERMINAL PROCEDURES CHARTS Selecting T erminal Procedur es Charts: While viewing the Navigation Map P age , Nearest Airport P age , or Flight Plan Page , select the SHW CHR T Softk ey . Or : 1) Press the MENU K ey to display the P AGE MENU . 2) T urn ...

  • Garmin G1000H - page 410

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 398 ADDITIONAL FEA TURES Whena chartis notavailable byselecting the SHW CHR T  Softkeyor selectingaPage MenuOption, charts maybeobtainedforotherairportsfromtheWPTPagesorFlightPlanPag ...

  • Garmin G1000H - page 411

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 399 ADDITIONAL FEA TURES While the APPROACH Box is selected using the FMS  Knob, the G1000H softkeys are blank.  Once the desiredchartisselected,thechartscalecanbechangedand thechart ...

  • Garmin G1000H - page 412

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 400 ADDITIONAL FEA TURES Selecting the INFO-1 or INFO-2 Softkeyr etur ns tothe airportdiagram chartwhen theview ison aterminal procedur e chart. Ifthe displayedchart is theairport diagramchart, sel ...

  • Garmin G1000H - page 413

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 401 ADDITIONAL FEA TURES In the example shown in Figure 8-26, the Class B Chart is selected.  Pressing the ENT  Key displays the CharlotteClassBAirspaceChart(Figure8-27). Figure 8-27 Airport Inform ...

  • Garmin G1000H - page 414

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 402 ADDITIONAL FEA TURES Selecting the ST AR SoftkeydisplaystheStandardT erminalArrivalChartifavailable. Change Range and Scroll Through the Chart With the Joystick Figure 8-29 Arrival Information P age Chart Not T o Scale Aircraft Not Shown Icon Sele ...

  • Garmin G1000H - page 415

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 403 ADDITIONAL FEA TURES Selecting the WX Softkeyshows theairportweatherfrequencyinformation, andincludesweatherdata such as MET AR and T AF from the XM Data Link Receiver , when available.  W eather? ...

  • Garmin G1000H - page 416

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 404 ADDITIONAL FEA TURES Figure 8-32 NO T AM Softkey Highlighted NO T AM Softkey Appears for Selected Airports Figure 8-33 Airport Information P age , Local NO T AMs Local NOT AM on This Airport NO T AM Softkey Selected Selecting the NOT AM Softkeyagainremovesthe ...

  • Garmin G1000H - page 417

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 405 ADDITIONAL FEA TURES CHART OPTIONS Selecting the CHR T OPT Softkeydisplaysthenextlevelofsoftkeys,thechartoptionslevel(Figure8-20). Selecting the ALL Softkeyshowsthecompleteapproachchartonthescr een. Figure 8-34 ...

  • Garmin G1000H - page 418

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 406 ADDITIONAL FEA TURES Selecting the HEADER Softkeyshowstheheaderview(approachchartbriengstrip)onthescr een. Approach Chart Briefing Strip Figure 8-35 Approach Information P age , Header View Selecting the PLAN Softkeyshowsthea ...

  • Garmin G1000H - page 419

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 407 ADDITIONAL FEA TURES Selecting the PROFILE Softkeydisplaystheapproachchartdescentpr olestrip. Approach Chart Descent Profile Strip Figure 8-37 Approach Information P age , Pr ofile View , Full Screen Width Selecting the MINIMUMS Softkeydispla ...

  • Garmin G1000H - page 420

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 408 ADDITIONAL FEA TURES If the chart scale has been adjusted to view a small area of the chart, selecting the FIT WIDTH  Softkey changesthechartsizetottheavailablescreenwidth. Select FIT ...

  • Garmin G1000H - page 421

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 409 ADDITIONAL FEA TURES Selecting the FULL SCN Softkeyalternatesbetweenremovingandreplacingthedatawindowtotheright. Selecting Additional Information: 1) While viewing the Airport T axi Diagram, select the FULL SCN Softk ey to display the inf ...

  • Garmin G1000H - page 422

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 410 ADDITIONAL FEA TURES Thefullscreenviewcanalsobeselectedbyusingthepagemenuoption. Selecting full screen On or Off: 1) While viewing a terminal chart press the MENU K ey to display the P age Menu OPTIONS . 2) T urn the large FMS Knob ...

  • Garmin G1000H - page 423

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 411 ADDITIONAL FEA TURES D A Y/NIGHT VIEW ChartViewcan bedisplayed ona whiteor black backgr ound for dayor nightviewing.  TheDay V iew offers abetter presentation ina brightenvironment. The? ...

  • Garmin G1000H - page 424

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 412 ADDITIONAL FEA TURES Figure 8-43 Arrival Information P age , Day View Figure 8-44 Arrival Information P age , Night View ...

  • Garmin G1000H - page 425

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 413 ADDITIONAL FEA TURES CHARTVIEW CYCLE NUMBER AND EXPIRA TION D A TE ChartViewdatabaseisr evisedevery14days. Chartsarestillviewableduringaperiodthatextendsfromthe cycle expiration date to the disables? ...

  • Garmin G1000H - page 426

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 414 ADDITIONAL FEA TURES The ChartV iew time critical information can also be found on the AUX-System Status page. The database CYCLEnumber , EXPIRES,andDISABLES datesofthe ChartV iew subscri ...

  • Garmin G1000H - page 427

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 415 ADDITIONAL FEA TURES Other possible AUX-System Status page conditions are shown in Figure 8-47.  The EXPIRES date is the revision date for the next database cycle.  The DISABLES date? ...

  • Garmin G1000H - page 428

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 416 ADDITIONAL FEA TURES 8.4 FLITECHARTS FliteChartsis anoptional featurer esemblingthepaper versionof AeroNav Servicesterminal procedures charts.  The charts are displayed with high-resolution and in co ...

  • Garmin G1000H - page 429

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 417 ADDITIONAL FEA TURES TERMINAL PROCEDURES CHARTS Selecting T erminal Procedur es Charts: While viewing the Navigation Map P age , Nearest Airport P age , or Flight Plan Page , select the SHW CHR T Softk ey . Or : 1) Press the MENU K ey to display the P AGE MENU . 2) T urn ...

  • Garmin G1000H - page 430

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 418 ADDITIONAL FEA TURES Whena chartis notavailable byselecting the SHW CHR T  Softkeyor selectingaPage MenuOption, charts maybeobtainedforotherairportsfromtheWPTPagesorFlightPlanPag ...

  • Garmin G1000H - page 431

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 419 ADDITIONAL FEA TURES While the APPROACH Box is selected using the FMS  Knob, the G1000H softkeys are blank.  Once the desired chart is selected, the chart scale can be changed and the? ...

  • Garmin G1000H - page 432

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 420 ADDITIONAL FEA TURES Selecting the INFO-1 or INFO-2 Softkeyr etur ns tothe airportdiagram chartwhen theview ison aterminal procedur e chart. Ifthe displayedchart is theairport diagramchart, sel ...

  • Garmin G1000H - page 433

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 421 ADDITIONAL FEA TURES In the example shown in Figure 8-54, T AKEOFF MINIMUMSis selected. Pressing the ENT  Key displaysthe T ake-offMinimumsandDeparturePr oceduresChart(Figure8-55). Figure 8-55 ...

  • Garmin G1000H - page 434

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 422 ADDITIONAL FEA TURES Selecting the ST AR SoftkeydisplaystheStandardT erminalArrivalChartifavailable. Figure 8-57 Arrival Information P age Selecting the APR Softkeydisplaystheapproachchartfortheairportifavailable. Figure ...

  • Garmin G1000H - page 435

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 423 ADDITIONAL FEA TURES Selecting the WX Softkey shows the airport weather frequency information, when available, and includes weatherdatasuchasMET ARandT AFfromtheXMDataLinkReceiver .W eatherinfo ...

  • Garmin G1000H - page 436

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 424 ADDITIONAL FEA TURES CHART OPTIONS Selecting the CHR T OPT Softkeydisplaysthenextlevelofsoftkeys,thechartoptionslevel(Figure8-48). Selecting the ALL Softkeyshowsthecompletechartonthescreen. Complete Chart Shown Fig ...

  • Garmin G1000H - page 437

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 425 ADDITIONAL FEA TURES Selecting the FIT WIDTH  Softkey ts the width of the chart in the display viewing area.  In the example shown,thechartatcloserangeisreplacedwiththefullwidthchar ...

  • Garmin G1000H - page 438

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 426 ADDITIONAL FEA TURES Selecting the FULL SCN Softkeyalternatesbetweenremovingandreplacingthedatawindowtotheright. Select FULL SCN Softkey to Switch Between Chart on Full Screen and Chart with Info Window Figure 8-62 Airport Information P a ...

  • Garmin G1000H - page 439

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 427 ADDITIONAL FEA TURES Thefullscreenviewcanalsobeselectedbyusingthepagemenuoption. Selecting full screen On or Off: 1) While viewing a terminal chart press the MENU K ey to display the P age Menu OPTIONS . 2) T urn the large FMS Knob ...

  • Garmin G1000H - page 440

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 428 ADDITIONAL FEA TURES D A Y/NIGHT VIEW FliteChartscan bedisplayedon awhiteor blackbackgroundfordayor nightviewing. TheDay V iew of fers abetter presentation ina brightenvironment. TheNi ...

  • Garmin G1000H - page 441

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 429 ADDITIONAL FEA TURES Figure 8-65 Approach Information P age , Day V iew Figure 8-66 Approach Information P age , Night V iew ...

  • Garmin G1000H - page 442

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 430 ADDITIONAL FEA TURES FLITECHARTS CYCLE NUMBER AND EXPIRA TION D A TE FliteCharts data is revised ever y 28 days.  Charts are still viewable during a period that extends from the cycle expirationdate tot ...

  • Garmin G1000H - page 443

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 431 ADDITIONAL FEA TURES Whenthe 180daygrace periodhas expired,‘Chartdata isdisabled.’in yellowindicates thattheFliteCharts database has expired and is no longer viewable.  ‘Chart Data: ...

  • Garmin G1000H - page 444

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 432 ADDITIONAL FEA TURES The FliteChartsdatabase is providedfromGarmin.  Refer toUpdating Garmin Databases inAppendixB for instructionsonrevisingtheFliteChartsdatabase. The otherthree possibleAUX? ...

  • Garmin G1000H - page 445

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 433 ADDITIONAL FEA TURES 8.5 A OP A AIRPORT DIRECT OR Y The Aircraft Owners and Pilots Association (AOP A) Airport Directory database offers detailed information regar ding services, hours of operation, lodging options ...

  • Garmin G1000H - page 446

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 434 ADDITIONAL FEA TURES A OP A D A T AB ASE CYCLE NUMBER AND REVISION The AOP A Airport Directory database is revised four times per year .  Check y .garmin.com for the current database.  The Airport Director ...

  • Garmin G1000H - page 447

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 435 ADDITIONAL FEA TURES The Airport Directory Region, V ersion, Cycle, Effective date andExpir esdate ofthe databasecycle canalso be found on the AUX-SystemStatuspage,asseeninFigure8-72. Select th ...

  • Garmin G1000H - page 448

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 436 ADDITIONAL FEA TURES 8.6 SA TELLITE TELEPHONE AND D A T A LINK SERVICES NO TE : Separate accounts must be established to access the Iridium satellite network for voice and Garmin Flight Data Services for data transmission of maintenance reports . The optional GDL? ...

  • Garmin G1000H - page 449

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 437 ADDITIONAL FEA TURES Figure 8-73 Report Status P age Selected Prior to System Registration 5) Press the MENU K ey . T he P age Menu window is now displayed as seen in Figure 8-74. 6) Select ‘Register With GFDS’ in the menu list. Figure 8-74 Select Register With GFDS ...

  • Garmin G1000H - page 450

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 438 ADDITIONAL FEA TURES 7) Press the ENT K ey . T he Garmin Flight Data Service Registration window is now displayed as shown in Figure 8-75. Figure 8-75 Enter Access Code 8) Enter the Access Code provided by Garmin Flight Data Services . 9) Press the ENT Ke y. REGISTER wil ...

  • Garmin G1000H - page 451

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 439 ADDITIONAL FEA TURES 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) T urn the large FMS Knob ...

  • Garmin G1000H - page 452

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 440 ADDITIONAL FEA TURES TELEPHONE COMMUNICA TION The pilot or copilot can place and answer calls on the Iridium satellite network.  Control and monitoring of  telephonefunctionsareaccomplishedthr oughth ...

  • Garmin G1000H - page 453

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 441 ADDITIONAL FEA TURES Internal Phone External Phone Description Phone is Idle Phone is ringing Phone has a dial tone (off hook) or connected to another phone Phone dialed is busy Phone is dialing another phone Phone has failed Phone status not known Phone is disabled Phon ...

  • Garmin G1000H - page 454

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 442 ADDITIONAL FEA TURES INCOMING CALLS NOTE: Outside callers should dial 00 + 8816 or 8817 + aircraft phone number when calling the aircraft Iridium T elephone System. When viewing MFD pages other than the AUX-TELEPHONE Page, a pop-up alert? ...

  • Garmin G1000H - page 455

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 443 ADDITIONAL FEA TURES Disabling incoming call alerts: 1) With the A UX-TELEPHONE P age displayed, press the MENU K ey on the MFD to display the P age Menu. 2) T urn either FMS Knob to place the cursor on ‘Disable Incoming Call Alerts’. 3) Press the ENT K ey . T he voi ...

  • Garmin G1000H - page 456

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 444 ADDITIONAL FEA TURES 4) Press the ENT K ey . ‘OK’ is highlighted as in Figure 8-82. Figure 8-82 Make the Call 5) Press the ENT K ey . T he system will begin calling the number , as in Figure 8-83. Figure 8-83 System is Making the Connection ...

  • Garmin G1000H - page 457

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 445 ADDITIONAL FEA TURES When thephone is answered,the connectionis established as shownin Figure 8-84. T oexit the call, select the HANGUP Softkey . Figure 8-84 Phone is Answered, Connection Complete ...

  • Garmin G1000H - page 458

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 446 ADDITIONAL FEA TURES PLA CING THE CALL ON HOLD T o place a call on hold: Select the HOLD Softk ey on the MFD . Or : 1) Press the MENU K ey to display the P age Menu. 2) T urn either FMS Knob to place the cursor on ‘Put Current Call On Hold’. 3) Press the ENT Ke y. Th ...

  • Garmin G1000H - page 459

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 447 ADDITIONAL FEA TURES TEXT MESSA GING (SMS) The pilot or copilot can send and receive text messages on the Iridium satellite network.  Messages may be sent to an email address or text message capable ...

  • Garmin G1000H - page 460

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 448 ADDITIONAL FEA TURES Message Symbol Description Received text message that has not been opened Received text message that has been opened Saved text message , draft not sent System is sending text message T ext message has been sent System failed to send text message Pre ...

  • Garmin G1000H - page 461

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 449 ADDITIONAL FEA TURES Figure 8-88 T ext Message Displayed from P op-Up Alert Thepop-upalertsmaybeenabledordisabledthroughthePageMenu. Enabling/disabling incoming text message pop-up alerts: 1) With the A UX-TEXT MESSAGING P age displayed, ...

  • Garmin G1000H - page 462

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 450 ADDITIONAL FEA TURES REPL Y T O A TEXT MESSA GE Afterreadingatextmessage,areplymaybesent. Replying to a text message: While viewing the text message , select the REPL Y Softk ey . Or : 1) Press the MENU K ey to display the P age Menu. 2) T urn ...

  • Garmin G1000H - page 463

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 451 ADDITIONAL FEA TURES 2) T he TEXT MESSAGE DRAFT Window is now displayed with the cursor in the ‘T O’ field. Enter 00 + country code + area code + phone number when sending to a text capable telephone . An email address may also be entered. Entry can be accomplished ...

  • Garmin G1000H - page 464

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 452 ADDITIONAL FEA TURES Or : a) Press the MENU K ey to display the Page Menu. b) T urn either FMS Knob to place the cursor on ‘Draft New Predefined Message’. c) Press the ENT Ke y. Th e PREDEFINED SMS TEXT MESSAGE Window is now displayed as shown in Figure 8-92. Figure ...

  • Garmin G1000H - page 465

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 453 ADDITIONAL FEA TURES Sending a predefined text message: 1) While viewing the A UX-TEXT MESSAGING P age , select the NEW Softk ey . 2) T he TEXT MESSAGE DRAFT Window is now displayed with the cursor in the ‘T O’ field. Enter the desired telephone number or email add ...

  • Garmin G1000H - page 466

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 454 ADDITIONAL FEA TURES 4) Select the PREDEFD Softkey . T he PREDEFINED MESSAGE MENU Window is displayed as seen in Figure 8-94. Figure 8-94 Predefined Message List 5) T urn either FMS Knob to select the desired predefined message . 6) Press the ENT K ey . T he predefine ...

  • Garmin G1000H - page 467

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 455 ADDITIONAL FEA TURES Figure 8-95 T ext Message Inbox Show Outbox messages: While viewing the A UX-TEXT MESSAGING P age , select the ARRANGE Softk ey , then select the OUTBO X Softk ey . Or : 1) Press the MENU K ey to display the P age Menu. 2) T urn either FMS Knob to pl ...

  • Garmin G1000H - page 468

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 456 ADDITIONAL FEA TURES MANA GING TEXT MESSAGES The viewedmessages maybe listed according tothe date/timethe message wassent orr eceived,the type of message(read,unread,sent,unsent,etc.),orbyme ...

  • Garmin G1000H - page 469

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 457 ADDITIONAL FEA TURES a) Press the MENU K ey to display the Page Menu. b) T urn either FMS Knob to place the cursor on ‘View Selected Message’. c) Press the ENT Ke y. Message content is displayed as shown in Figure 8-96. Figure 8-96 Viewing Message Content 5) T o clos ...

  • Garmin G1000H - page 470

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 458 ADDITIONAL FEA TURES Marking all messages as read: 1) While viewing the Inbox on the A UX-TEXT MESSAGING P age , press the MENU Key to display the P age Menu. 2) T urn either FMS Knob to place the cursor on ‘Mark All New Messages As Read’. 3) Press the ENT K ey . A c ...

  • Garmin G1000H - page 471

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 459 ADDITIONAL FEA TURES T o set up a new Wi-Fi connection: 1) Select the AVA I L Softk ey on the MFD. A list of available networks will be displayed in the A V AILABLE NETWORKS window as shown in Figure 8-97. Signal strength is shown for each network, as well as security re ...

  • Garmin G1000H - page 472

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 460 ADDITIONAL FEA TURES 4) T urn either FMS Knob to select the desired network. See Figure 8-98. Figure 8-98 Desired Network Selected 5) Select the CONNECT Softk ey . Or : a) Press the MENU K ey to display the Page Menu. b) T urn either FMS Knob to place the cursor on ‘Co ...

  • Garmin G1000H - page 473

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 461 ADDITIONAL FEA TURES 7) Press the ENT K ey . ‘OK’ will be highlighted. 8) Press the ENT K ey again. 9) T he SA VE SETTINGS window is now displayed with the cursor highlighting ‘SA VE CONNECTION’. Figure 8-100 Save Option 10) T he selected network can be saved to ...

  • Garmin G1000H - page 474

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 462 ADDITIONAL FEA TURES T o edit a saved network: 1) While viewing list of saved networks , press the FMS Knob to activate the cursor as seen in Figure 8-102. 2) T urn either FMS Knob to highlight the network to be edited. 3) Pressing the ENT K ey at this point will check o ...

  • Garmin G1000H - page 475

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 463 ADDITIONAL FEA TURES 4) Select the EDIT Softk ey . T he cursor now appears in the CONNECTION SETTINGS window as shown in Figure 8-103. Figure 8-103 Select Attributes to Edit 5) T urn the large FMS Knob to select the network attribute to be edited. 6) T urn the small FMS ...

  • Garmin G1000H - page 476

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 464 ADDITIONAL FEA TURES SY STEM D A T A LOGGING NO TE : An account must be established with Garmin Flight Data Services to mak e full use of the System Data Logging feature . Thesystem provides recording ofCAS andCMC messagesthat occurwhile? ...

  • Garmin G1000H - page 477

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 465 ADDITIONAL FEA TURES T o change transmission method: 1) While viewing the Report Status P age , press the FMS Knob to activate the cursor . 2) T urn the large FMS Knob to move the cursor to the 1st or 2nd tr ansmit method for the desired data report. 3) T urn the small F ...

  • Garmin G1000H - page 478

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 466 ADDITIONAL FEA TURES T o send a transmission manually: NO TE : Manual transmission of data can only be performed while the aircraft is on the ground. 1) While viewing the Report Status P age , press the FMS Knob to activate the cursor . 2) T urn the large FMS Knob to mov ...

  • Garmin G1000H - page 479

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 467 ADDITIONAL FEA TURES 8.7 XM RADIO ENTERT AINMENT NOTE: Refer to the Hazard Avoidance Section for information about XM Weather products . Theoptional XMRadio entertainmentfeatur eofthe GDL69AData LinkReceiver isavailable for ...

  • Garmin G1000H - page 480

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 468 ADDITIONAL FEA TURES 6) Select the LOCK Softk ey . 7) T urn the large FMS Knob to highlight YES. 8) T o complete activation, press the ENT Ke y. RADIO and INFO Softkeys Figure 8-108 XM Information P age Audio Radio ID Weather Products Window Data Radio ID LOCK Softkey is ...

  • Garmin G1000H - page 481

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 469 ADDITIONAL FEA TURES Figure 8-109 XM Radio P age V olume Field Categories Field Channel List Active Channel A CTIVE CHANNEL AND CHANNEL LIST The ActiveChannel Boxon the XMRadio Pagedisplays the currentlyselected channelthat th ...

  • Garmin G1000H - page 482

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 470 ADDITIONAL FEA TURES CA TEGOR Y The Category Box of the XM Radio Page displays the currently selected category of audio. Categories of channelssuchas jazz,r ock,ornewscanbeselected tolist ...

  • Garmin G1000H - page 483

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 471 ADDITIONAL FEA TURES PRESETS Up to15 channelsfr omany categor y canbe assigneda presetnumber . The preset channelsare selectedby selecting the PRESETS and MORE Softkeys.Thenthepr esetchannel ...

  • Garmin G1000H - page 484

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 472 ADDITIONAL FEA TURES 8.8 SCHEDULER The Scheduler feature can be usedto enter and display reminder messages (e.g., Phase 1 Inspection, Switch fuel tanks,orAltimeter -T ransponderCheck)intheAlertsWindo ...

  • Garmin G1000H - page 485

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 473 ADDITIONAL FEA TURES 9) F or event-based messages: a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press the ENT Ke y. b) Press the ENT K ey again or use the large FMS Knob to move the cursor to the next field. c) Use the FMS Knob to enter the desired time ...

  • Garmin G1000H - page 486

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 474 ADDITIONAL FEA TURES 8.9 A UXILIARY VIDEO The G1000H system provides an optional contr ol and display interface to an auxiliary video system.  The systemcandisplayvideoforuptotwoinputs. Therear ...

  • Garmin G1000H - page 487

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 475 ADDITIONAL FEA TURES Selecting video menu options: 1) While viewing the A UX - VIDEO P age press the MENU K ey to display the P age Menu OPTIONS . 2) T urn the large FMS Knob to highlight the desired video adjustment option and press the ENT Ke y. Oncethe ENT ke ...

  • Garmin G1000H - page 488

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 476 ADDITIONAL FEA TURES DISPLA Y SELECTION Pressing the HIDE MAP  Softkey removes the map and displays video on the full screen.  The softkey label changes to grey with black characters.  Pressing ...

  • Garmin G1000H - page 489

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 477 ADDITIONAL FEA TURES INPUT SELECTION Whileonthe AUX-VIDEOPage,pressthe INPUT  SoftkeytoselectInput1 orInput2.The selectedinput isdisplayedintheupperleftofthevideodisplay . ZOOM/R ...

  • Garmin G1000H - page 490

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 478 ADDITIONAL FEA TURES 8.9 ABNORMAL OPERA TION SVS TROUBLESHOO TING SVS is intended to be used with traditional attitude, heading, obstacle, terrain, and trafc inputs.  SVS is disabled when valid attitude ...

  • Garmin G1000H - page 491

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 479 ADDITIONAL FEA TURES UNUSU AL A TTITUDES Unusual attitudes are displayed with red chevrons overlaid on the display indicating the direction to y to correct the unusual attitude condition.  The dis ...

  • Garmin G1000H - page 492

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 480 ADDITIONAL FEA TURES GDL 69H/69AH D A T A LINK RECEIVER TROUBLESHOO TING Somequicktroubleshootingstepslistedbelowcanbeperformedtondthepossiblecauseofafailur e. • Ensuretheowner/operatoroftheair craft? ...

  • Garmin G1000H - page 493

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 481 ADDITIONAL FEA TURES Ifafailurestillexists,thefollowingmessagesmaypr ovideinsightastothepossibleproblem: Message Message Location Description CHECK ANTENNA XM Radio P age - active channel field Data Link Receiver antenna erro ...

  • Garmin G1000H - page 494

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 482 ADDITIONAL FEA TURES B lank P age ...

  • Garmin G1000H - page 495

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 483 APPENDIX A ANNUNCIA TIONS AND ALERTS CAS MESSA GES W ARNING MESSAGES See the Rotorcraft Flight Manual (RFM) for r ecommended pilot actions. Annunciation T ext Description Audio Alert B A TTER Y HO T Battery overheat detected. Single Chime ENGINE FIRE Fire/Overheat detect ...

  • Garmin G1000H - page 496

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 484 APPENDIX A Annunciation T ext Description Audio Alert MGT MISCOMP MGT miscompare event. Single Ping NG EXCEED Engine Ng is in exceedance. NG MISCOMP Ng miscompare event. NP EXCEED Engine NP is in exceedance . NP MISCOMP NP miscompare event. NR MISCOMP NR miscompare event ...

  • Garmin G1000H - page 497

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 485 APPENDIX A G1000H SYSTEM ANNUNCIA TIONS When a new message is issued, the MSG Softkey will flash to alert the flight crew of a new message. It will continue to flash until acknowledged by pressing the softkey . Active messages are displayed in white text. Messages tha ...

  • Garmin G1000H - page 498

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 486 APPENDIX A Figure A-2 G1000H System F ailure Annunciations GDC 74B Air Data Computer GTX 33/D T ransponder Or GIA 63W Integrated Avionics Units GDC 74B Air Data Computer GEA 71 Engine Airframe Unit Or GIA 63W Integrated Avionics Unit GIA 63W Integrated Avionics Units GRS ...

  • Garmin G1000H - page 499

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 487 APPENDIX A System Annunciation Comment Display system is not receiving airspeed input from air data computer . Display system is not receiving valid heading input from AHRS . Display system is not receiving altitude input from the air data computer . Display system is no ...

  • Garmin G1000H - page 500

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 488 APPENDIX A HT AWS ALERTS Alert T ype PFD/HT A WS P age Alert Annunciation MFD P op-Up Alert (except HT A WS P age) Aural Message Reduced Required T errain Clear ance W arn ing (R TC) “W arning; T errain, T errain” Imminent T errain Impact W arning (ITI) “W arning; ...

  • Garmin G1000H - page 501

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 489 APPENDIX A Alert T ype PFD/HT A WS P age Status Annunciation HT A WS P age Center Banner Annunciation Aural Message T errain or Obstacle database unav ailable or invalid on all displays , inv alid software configuration, HT AWS audio fault HT A WS F AIL “HT AWS F ailu ...

  • Garmin G1000H - page 502

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 490 APPENDIX A G1000H SY STEM MESSA GE ADVISORIES NOTE: T his Section provides information regarding G1000H message advisories that may be displayed by the system. Knowledge of the aircraft, systems , flight conditions , and other existing operational priorities must be con ...

  • Garmin G1000H - page 503

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 491 APPENDIX A D A T ABASE MESSA GE ADVISORIES Message Comments MFD1 DB ERR – MFD1 navigation database error exists . T he MFD and/or PFD detected a failure in the navigation database . Attempt to reload the navigation database . If problem persists, the system should be s ...

  • Garmin G1000H - page 504

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 492 APPENDIX A D A T ABASE MESSA GE ADVISORIES (CONT .) Message Comments DB MISMA TCH – T errain database mismatch. T he PFDs and MFD have different terrain database versions or types installed. Install correct terrain database version or type in all displays . DB MISMA TC ...

  • Garmin G1000H - page 505

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 493 APPENDIX A GIA 63H MESSA GE ADVISORIES (CONT .) Message Comments GIA1 COOLING – GIA1 over temperature . The GIA1 and/or GIA2 temper ature is too high. If problem persists, the system should be serviced. GIA2 COOLING – GIA2 over temperature . GIA1 SER VICE – GIA1 ne ...

  • Garmin G1000H - page 506

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 494 APPENDIX A GIA 63H MESSA GE ADVISORIES (CONT .) Message Comments GPS NA V LOST – Loss of GPS navigation. P osition error . Loss of GPS navigation due to position error . GPS NA V LOST – Loss of GPS navigation. GPS fail. Loss of GPS navigation due to GPS failure . ABO ...

  • Garmin G1000H - page 507

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 495 APPENDIX A GTX 33H MESSA GE ADVISORIES Message Comments XPDR1 CONFIG – XPDR1 config error . Config service req’ d. T he transponder configur ation settings do not match those of backup configuration memory . T he system should be serviced. MANIFEST – GTX1 softw ...

  • Garmin G1000H - page 508

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 496 APPENDIX A GSR 56H MESSA GE ADVISORIES Message Comments GSR1 F AIL – GSR1 has failed. A failure has been detected in the #1 GSR 56H. The system should be serviced. GDL 59H MESSA GE ADVISORIES Message Comments GDL59 CONFIG – GDL 59 config error . Config service req? ...

  • Garmin G1000H - page 509

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 497 APPENDIX A GDC 74H MESSA GE ADVISORIES Message Comments ADC1 AL T EC – ADC1 altitude error correction is unavailable . GDC is reporting that the altitude error correction is unavailable . ADC1 AS EC – ADC1 airspeed error correction is unavailable . GDC is reporting t ...

  • Garmin G1000H - page 510

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 498 APPENDIX A MISCELLANEOUS MESSA GE ADVISORIES (CONT .) Message Comments WPT ARRIV AL – Arriving at waypoint -[xxxx] Arriving at waypoint [xxxx], where [xxxx] is the waypoint name . STEEP TURN – Steep turn ahead. A steep turn is 15 seconds ahead. Prepare to turn. INSID ...

  • Garmin G1000H - page 511

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 499 APPENDIX A MISCELLANEOUS MESSA GE ADVISORIES (CONT .) Message Comments MA G V AR WARN – Large magnetic variance . V erify all course angles . T he GDU’ s internal model cannot determine the exact magnetic variance for geogr aphic locations near the magnetic poles . D ...

  • Garmin G1000H - page 512

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 500 APPENDIX A Flight Plan Import/Export Results Description ‘Some waypoints not loaded. W aypoints locked. ’ The flight plan on the SD card contains one or more w aypoints that the system cannot find in the navigation database . T he flight plan has been imported, bu ...

  • Garmin G1000H - page 513

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 501 APPENDIX B D A T ABASE MANA GEMENT CAUTION: Never disconnect power to the system when loading a database. P ower interuption during the database loading process could result in maintenance being required to reboot the system. The system uses Secure Digital (SD) car ds to ...

  • Garmin G1000H - page 514

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 502 APPENDIX B Updating the active Jeppesen navigation database (not using the Dual Navigation Database or Automatic Database Synchronization F eatures): 1) With the system OFF , insert the SD card containing the new navigation database version into the top card slot of the ...

  • Garmin G1000H - page 515

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 503 APPENDIX B DU AL NA VIGA TION D A T AB ASE FEA TURE The dual navigation database feature allows each display to store an upcoming navigation database on the bottom SD card so that the system can automatically load it to r eplace the active database when the new database ...

  • Garmin G1000H - page 516

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 504 APPENDIX B 5) After the navigation database files are copied to the bottom SD card, the display will appear as shown in Figure B-4. Figure B-4 Standby Navigation Database Update Complete 6) As instructed on the display , press any k ey to continue . T he display will no ...

  • Garmin G1000H - page 517

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 505 APPENDIX B 13) T urn system power OFF . 14) Remove the SD card from the top card slot of the MFD . 15) T urn system power ON . 16) Press the ENT K ey to acknowledge the startup screen. 17) T urn the large FMS Knob to select the A UX P age group on the MFD . 18) T urn the ...

  • Garmin G1000H - page 518

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 506 APPENDIX B Since these databases are not stored internally in the displays, a Supplemental Data Car d containing identical database versions must be kept in each display unit. The basemap database contains data for the topography and land features, such as rivers, lakes, ...

  • Garmin G1000H - page 519

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 507 APPENDIX B The synchronization pr ogress may be monitored on the AUX-System Status Page in the Sync Status section of the Database W indow (Figure B-8). This section shows the synchronization status of each applicable database, including the percent complete, time r emai ...

  • Garmin G1000H - page 520

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 508 APPENDIX B 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 pr ...

  • Garmin G1000H - page 521

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 509 APPENDIX B Figure B-10 Database Information on the P ower -up Screen 5) Acknowledge the P ower -up P age agreement by pressing the ENT K ey or the right most softk ey . 6) T urn the large FMS Knob to select the A UX Page group on the MFD . 7) T urn the small FMS Knob to ...

  • Garmin G1000H - page 522

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 510 APPENDIX B MA GNETIC FIELD V ARIA TION D A T AB ASE UPD A TE A copy of the current magnetic field variation database (MV DB) is included with the navigation database. At startup, the system compares this version of the MV DB with that presently being used by the AHRS (G ...

  • Garmin G1000H - page 523

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 511 APPENDIX C ACC accur acy ACT , A CTV active , activ ate ADC air data computer ADF Automatic Direction Finder ADI Attitude Direction Indicator AF Arc to fix AFCS Automatic Flight Control System AFRM airframe AGL Above Ground Level AHRS Attitude and Heading Reference Syst ...

  • Garmin G1000H - page 524

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 512 APPENDIX C DEC FUEL decrease fuel deg degree DEIC , DEICE de-icing DEP departure Desired T rack The desired course between the active “from” and “to” waypoints . DEST destination DF Direct to Fix DFL T default DGRD degrade DH decision height Dilution of Precision ...

  • Garmin G1000H - page 525

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 513 APPENDIX C GA go-around gal, gl gallon(s) GBOX gearbox GDC Garmin Air Data Computer GDU Garmin Display Unit GEA Garmin Engine/Airframe Unit GEO geographic GFC Garmin Flight Control GIA Garmin Integrated Avionics Unit GLS Global Navigation Satellite Landing System GMA Gar ...

  • Garmin G1000H - page 526

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 514 APPENDIX C Leg The portion of a flight plan between two waypoints . LIFR Low Instrument Flight Rules LNA V Later al Navigation LO low LOC localizer LOI loss of integrity (GPS) LON longitude LPV Localizer Performance with V ertical guidance LRU Line Replaceable Unit L T ...

  • Garmin G1000H - page 527

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 515 APPENDIX C RFM Rotorcraft Flight Manual RFM S Rotorcraft Flight Manual Supplement RMI Radio Magnetic Indicator RMT remote RNG range RNWY runway ROL roll ROM read only memory rpm revolutions per minute RST FUEL reset fuel RSV reserve (fuel reserve entered by pilot) R T ri ...

  • Garmin G1000H - page 528

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 516 APPENDIX C V ertical Speed Required T he vertical speed necessary to descend/ climb from a current position and altitude to a defined target position and altitude , based upon current groundspeed. VFOM V ertical Figure of Merit VFR V isual Flight Rules VHF V ery High Fr ...

  • Garmin G1000H - page 529

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 517 APPENDIX D FREQUENTL Y ASKED QUESTIONS If a particular aspect of G1000H operational capability is not addressed by these commonly asked questions or in the index, contact Garmin (see the copyright page or back cover for contact information) or a Garmin- authorized dealer ...

  • Garmin G1000H - page 530

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 518 APPENDIX D For RAIM to work correctly , the GPS receiver must track at least five satellites. A minimum of six satellites is required to allow RAIM to eliminate a single corrupt satellite fr om the navigation solution. RAIM ensures that satellite geometry allows for a n ...

  • Garmin G1000H - page 531

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 519 APPENDIX D Normal (OBS not activated) • Automatic sequencing of waypoints • ManualcoursechangeonHSInotpossible • Alwaysnavigates‘TO’theactivewaypoint • Mustbeinthismodefornalapproach cour ...

  • Garmin G1000H - page 532

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 520 APPENDIX D w hen DOes the cDi scale change ? Once adeparture is activated, theCourse DeviationIndicator (CDI) full scaledeection isset to 0.3 nm. The CDI scale changes to 1.0 nm (terminal mode) then ramps up ...

  • Garmin G1000H - page 533

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 521 APPENDIX E GENERAL TIS INFORMA TION INTRODUCTION NO TE : Aircraft without an operating transponder are invisible to TIS . The T raffic Information Service (TIS) provides traffic advisory information to non-T AS/TCAS-equipped aircraft. TIS is a gr ound-based service pro ...

  • Garmin G1000H - page 534

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 522 APPENDIX E W ARNING : Garmin is not responsible for Mode S geographical coverage . Operation of the ground stations is the responsibility of the F AA. Refer to the AIM for a T erminal Mode S radar site map . NO TE : TIS is unavailable at low altitudes in many areas of th ...

  • Garmin G1000H - page 535

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 523 APPENDIX F AIRPOR T Item Symbol Unknown Airport Non-towered, Non-serviced Airport T owered, Non-serviced Airport Non-towered, Serviced Airport T owered, Serviced Airport Restricted (Private) Airport Heliport NA V AIDS Item Symbol Intersection LOM (compass locator at oute ...

  • Garmin G1000H - page 536

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 524 APPENDIX F LINE SYMBOLS Item Symbol ICAO Control Area Class B Airspace Mode C Tower Area W arning Area Alert Area Caution Area Danger Area Prohibited Area Restricted Area T raining Area Unknown Area Class C T erminal Radar Service Area Mode C Area Military Operations Are ...

  • Garmin G1000H - page 537

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 525 APPENDIX F OBST ACLE D A T AB ASE Unlighted Obstacle Lighted Obstacle Obstacle Location < 1000’ AGL > 1000’ A GL < 1000’ AGL > 1000’ A GL Red obstacle is at or above current aircraft altitude Y ellow obstacle is between 0’ and 250’ below current a ...

  • Garmin G1000H - page 538

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 526 APPENDIX F MISCELLANEOUS Item Symbol AR TCC F requency or FSS F requency Default Map P ointer Elevation P ointer Wind V ector Measuring P ointer Overzoom Indicator T errain Proximity or T AWS Enabled T raffic Enabled User W aypoint V ertical Navigation Along T rack W ay ...

  • Garmin G1000H - page 539

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 527 APPENDIX F TELEPHONE SYMBOLS Internal Phone External Phone Description Phone is Idle Phone is ringing Phone has a dial tone (off hook) or connected to another phone Phone dialed is busy Phone is dialing another phone Phone has failed Phone status not known Phone is disab ...

  • Garmin G1000H - page 540

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 528 APPENDIX F B lank P age ...

  • Garmin G1000H - page 541

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX I-1 INDEX A Access code ------------------------------------------------- 438 Activate a Flight Plan -------------------------------------- 217 Active channel ---------------------------------------------- 469 Active database ------------------------------------- 502, 503 Ac ...

  • Garmin G1000H - page 542

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B I-2 INDEX Datalink receiver troubleshooting ----------------------- 480 Data report--------------------------------------------------- 29 Data reports ----------------------------------- 464, 465, 466 Date and time ----------------------------------------------- 32 Day/Night ...

  • Garmin G1000H - page 543

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX I-3 INDEX Indicated Altitude ------------------------------------------ 248 Initialization (system) --------------------------------------- 11 Intersection Information --------------------------------------- 177–178 Inverting a flight plan -------------------------------- ...

  • Garmin G1000H - page 544

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B I-4 INDEX Reduced Protection Mode -------------------------------- 346 Register ----------------------------------------------- 436, 438 Report transmissions -------------------------------------- 464 Required V ertical Speed ------------------------------------------- 272 V ...

  • Garmin G1000H - page 545

    190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX I-5 INDEX V V ertical deviation guidance ------------------------------ 234 V ertical Deviation Indicator (VDI) ------------- 55, 272, 273 V ertical navigation ----------------------------------------- 233 Direct-to -------------------------------------------------- 232 V er ...

  • Garmin G1000H - page 546

    Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B I-6 INDEX B lank P age ...

  • Garmin G1000H - page 547

    ...

  • Garmin G1000H - page 548

    Garmin International, Inc. 1200 East 151st Street Olathe , KS 66062, U .S .A. p:913.397.8200 f:913.397.8282 www .garmin.com Garmin A T , Inc . 2345 T urner Road SE Salem, OR 97302, U .S .A. p:503.391.3411 f:503.364.2138 Garmin (Europe) Ltd. Liberty House , Bulls Copse Road Houndsdown Business P ark Southampton, SO40 9RB , U .K. p:44/0870.8501241 f: ...

Manufacturer Garmin Category Marine Radio

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All of them are important, but the most important information from the point of view of use of the device are in the user manual Garmin G1000H.

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A manual, also referred to as a user manual, or simply "instructions" is a technical document designed to assist in the use Garmin G1000H by users. Manuals are usually written by a technical writer, but in a language understandable to all users of Garmin G1000H.

A complete Garmin manual, should contain several basic components. Some of them are less important, such as: cover / title page or copyright page. However, the remaining part should provide us with information that is important from the point of view of the user.

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2. Contents - index of all tips concerning the Garmin G1000H, that we can find in the current document
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