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G1000H ™ Integrated Flight Deck Pilot’ s Guide Bell 407GX.
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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 .
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.
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 .
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 .
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 .
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 , .
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) ..................
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) .
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 .
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B x T ABLE OF CONTENTS B lank P age.
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.
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.
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.
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.
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 .
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.
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 .
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.
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.
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.
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 .
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 .
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 .
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 .
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.
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 .
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 configuration.
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 D.
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.
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 .
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 declutte.
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).
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: • Satelliteconstellationdiagram Satellites currently in view are shown at their r espective positions on a sky view diagram.
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.
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.
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.
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.
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 optiona.
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 - Syste.
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 .
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.
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.
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.
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.
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 .
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.
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.
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 .
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.
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 .
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.
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.
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.
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 .
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 ’.
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 46 SY STEM OVER VIEW B lank P age.
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 .
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 .
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 In.
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.
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 51 FLIGHT INSTRUMENTS A TTITUDE INDICA T OR Attitude information isdisplayed over a virtual blue sky andbrown gr ound with a white horizon line.
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.
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 metricunitsar eselected.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 54 FLIGHT INSTRUMENTS ABaroT ransitionAlertisprovidedtoalertthepilottochangethebarometricpr essuresettingwhencrossing the transition altitude in either direction.
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 .
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.
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.
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 -.
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.
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.
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 61 FLIGHT INSTRUMENTS HEADING PRESET MODE HeadingPresetModeallowsAHRSto computeheadingdatawithoutusingthemagneticsensingdevice.
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.
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 .
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.
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.
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.
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.
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.
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 .
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 70 FLIGHT INSTRUMENTS WIND D A T A W inddirectionandspeed(relativetotheair craft)inknotscanbedisplayedinawindowtotheupperleftof theHSI.
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 aVNV ight planhas been activated,.
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 aredisplayed on the PFD.
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 73 FLIGHT INSTRUMENTS TRAFFIC ANNUNCIA TION T rafc is displayed symbolically on the PFD Inset Map, the MFD Navigation Map Page, and various other MFD page maps.
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.
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 MinimumDescent Altitude (MDA) or DecisionHeight (DH), based on bar ometric altitude or radar altitude, can be set.
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 le.
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 77 FLIGHT INSTRUMENTS A gr ound line (Figure2-49) is shownon the Altimeter todisplay the air craft’ s height relativeto the gr ound.
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 TheannunciationslistedinT able2-3canappearonthe HSIwhenabnormalGPSconditionsoccur .
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.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev B 80 FLIGHT INSTRUMENTS B lank P age.
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 .
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).
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.
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 Figu.
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 .
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.
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 .
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.
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 .
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 U.
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.
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.
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 .
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 Box.
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.
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.
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.
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.
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 .
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.
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: •.
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 CO.
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 scrollingthrough the list.
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-tunedfr om the NRST–Nearest Air.
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 TheCOM radioscantuneeither 25-kHzspacing(118.000 to136.975MHz) or8.33-kHzspacing (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.
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.
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.
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 totransfer thefrequency tuningbox andFrequency T ransferArr owbetween the upper and lower radio frequency fields.
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 Vfrequenciescanbeselectedandloaded.
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 .
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, theVOR 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.
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.
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.
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 . Themarker beaconreceiveris usedas partof theILS.
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 .
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 TheGTX33ModeST ransponderprovidesModeA,ModeC,and Mode S interr ogation and reply capabilities.
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.
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 .
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 .
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 .
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 .
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-testduring power -up.
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 .
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 .
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.
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.
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.
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.
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 .
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.
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 .
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.
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”.
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.
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.
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 hav.
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 associatedequipment,includingswitchesandexternaldevices.
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.
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 - Fligh.
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.
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.
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.
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.
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 145 FLIGHT MANA GEMENT • The ‘time out’ time (congurable on the Map Setup Page for the Map Group) determines how long auto zoom is overridden by a manual adjustment of the range knob.
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: • Viewpartsofthemapoutsidethed.
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.
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 .
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.
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.
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 p.
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.
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.
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 Aircr.
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.
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 .
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.
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 .
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.
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 .
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.
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.
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.
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.
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.
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.
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.
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.
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.
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 Du.
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 R.
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/Regio.
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.
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.
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.
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 .
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.
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.
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.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 180 FLIGHT MANA GEMENT TheNearestNDB Pagecan beused toquicklynd aNDB closeto theightpath.
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 aNA V receiver), or to quicklyauto-tune a VOR or ILS frequency .
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.
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.
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 W.
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.
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.
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.
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.
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).
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.
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.
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 .
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 .
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 Acti.
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 .
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.
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.
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.
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.
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: • Airwayidentier ,entrywaypointorexitwaypointnotfoundinthenewdatabase.
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 .
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 .
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 .
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.
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.
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.
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.
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 .
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.
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.
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 Depar.
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.
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 r.
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.
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.
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.
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.
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.
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 .
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 .
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 .
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.
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.
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 a.
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.
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).
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.
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 .
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.
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).
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.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 232 FLIGHT MANA GEMENT Cancelingverticalnavigationresultsinverticaldeviation (VDEV),verticalspeedrequired(VSREQ),andtime to top of descent/bottom of descent (TIME TO TOD/BOD) going invalid.
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 .
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.
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 235 FLIGHT MANA GEMENT An altitude constraint is invalid if: • Meetingtheconstraintrequirestheair craft.
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 .
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.
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 Depart.
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 .
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.
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 .
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.
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.
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 Approa.
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 .
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 .
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 .
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.
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.
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.
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.
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.
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.
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’.
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.
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.
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.
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 .
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.
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.
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.
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.
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.
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 .
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 .
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 .
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.
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.
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.
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.
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.
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 .
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.
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.
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 .
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 276 FLIGHT MANA GEMENT Figure 5-137 Approaching PYNON.
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 .
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.
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 .
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.
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.
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.
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 283 FLIGHT MANA GEMENT 5.12 ABNORMAL OPERA TION ThissectiondiscussestheDeadReckoningmodeofoperationandthesubsequentindications. NO TE: Dead Reck oning Mode only functions in Enroute (ENR) or Oceanic (OCN) phase of flight.
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 Reckon.
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.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 286 HAZARD A VOID ANCE SiriusXMusesthecodedIDsto sendanactivationsignalthatallowsthesystemto displayweatherdataand/ orentertainmentprogrammingpr ovidedthroughtheGDL69AH.
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 .
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.
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 289 HAZARD A VOID ANCE T able6-2showswhichXMWXproductscanbedisplayed(indicatedwitha‘+’symbol)onspecicmaps.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 290 HAZARD A VOID ANCE Softkeyscontrolthedisplay ofweatherinformation onmostMFD pagesandthe PFDInsetMap (Figure6-3 shows the weather pr oduct softkeys for the W eatherData Link (XM)Page).
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).
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 292 HAZARD A VOID ANCE Mapsbesides theW eather DataLink(XM) Pageuse settingsbasedon thoseselectedfor theNavigation Map Page.
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 .
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.
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 .
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 296 HAZARD A VOID ANCE neXRaD l imit a tiOns NEXRADradarimagesmayhavecertainlimitations: • NEXRAD b.
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 ) • Radarcoverageextendsto55ºN. • Anyprecipitationdisplayedbetween52ºNand55ºNisdisplayedasmixedbecauseitisunknown.
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 (Figure6-14) shows the location, elevation, and direction ofthe highest radar echo.
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.
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) showsthe approximate location of cloud-to-ground lightning strikes.
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 identied by the ground-based system.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 302 HAZARD A VOID ANCE SIGMETS AND AIRMETS SIGMET (SIGnicantMET eor ological Information) and AIRMET (AIRmen’ s MET eorologicalInformation) are issued for potentially hazar dous weather .
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).
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.
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 .
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.
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 isothermis found(Figur e6-30).
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.
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 specic public awareness and protection weather warnings from the National W eather Ser vice (NWS).
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,andtheirprojectedtracks.
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).
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) identies the potential for erratic movement of high-altitude air mass associatedwinds.
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) describein-ight weatherencounter edby pilots.
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 Selec.
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 .
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 inf.
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.
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 specic G1000H maps.
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.
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 .
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 321 HAZARD A VOID ANCE If both GFDSand XM weather services areinstalled, customizing the dis.
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 Navigati.
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 Poi.
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 .
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 Pre.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 326 HAZARD A VOID ANCE Atthecompletionofasuccessfulweatherdatarequest,therequeststatuswindow(ifstillopen)willindicate ‘OK’.
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.
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 .
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 Thefollowingmaycauseabnorm.
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 .
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 lightningstrikes.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 332 HAZARD A VOID ANCE SIGMETS AND AIRMETS SIGMET s (SIGnicant MET eorological Information) and AIRMET s (AIRmen’ s MET eor ologicalInformation) are issued for potentially hazar dous weather .
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.
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 .
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 whentheMET ARtextdoesnotcontainadequateinformation.
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.
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.
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 requeststatuswindow .
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 339 HAZARD A VOID ANCE TheG1000H alsodisplaysmessageadvisories onthePFD whichmayindicate apr oblemwiththe GDL59H; refertoAppendixAformoreinformation.
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 .
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 fromthebar o-correctedaltitude.
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 Pageis specialized toshow terrain,obstac.
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 Cur.
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.
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 Messag.
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.
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).
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.
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 systempower -up, HT A WS conducts asystem-test of itsaural and visual annunciations. The system test can also be manually initiated.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 350 HAZARD A VOID ANCE ‘HT A WSN/A ’isgeneratedintheannunciationwindowand ontheHT A WSPage.Theauralmessage “HT A WS Not A vailable” isalso generated.
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 .
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 rafcinformationcanbedisplayedonthefollowingmap.
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).
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 trafc.
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 355 HAZARD A VOID ANCE TIS ALERTS WhenthenumberofT AsontheT rafcMapPageincreasesfromonescantothenext,thefollowingoccur: • Asingle “T raffic” voice alert is generated.
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 TheG1000H performs anautomatic testof TISduring power -up.
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.
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.
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 8.
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 trafcwithanupwardordownwar d-pointingarrowr espectively .
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.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 362 HAZARD A VOID ANCE AT Awillbedisplayed foratleasteightseconds, evenifthe condition(s)thatinitially triggeredthe T Aareno longer present.
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’.
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’.
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 trafc is displayed.
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 rafc Map Page (Figure 6-96).
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 .
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 rafcinformationcanbedisplayedonthefollowing.
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).
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 370 HAZARD A VOID ANCE The Navigation Map Page SetupMenu also controls the display of trafc. The setup menu controls the map range settings.
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 371 HAZARD A VOID ANCE Theannunciations toindicatethe statusof trafcinformation appearina bannerat thelower leftcornerof mapsonwhichtrafccanbedisplayed.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 372 HAZARD A VOID ANCE B lank P age.
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 ™ 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 ™ 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.
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 .
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 isactivated fromthe PFD usingthe softkeys locatedalong the bottom edgeof the display .
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.
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 .
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 o.
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 showndescending only fora pr ogrammed descent(Figur es8-5, 8-6).
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 382 ADDITIONAL FEA TURES m isseD a PPROa ch Upon activatingthe missed approach, pathways leadto the.
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.
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 ZeroPitch Line.
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.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 386 ADDITIONAL FEA TURES HT AWS ALER TING T errainalertingonthesyntheticterrain displayistriggered byForward-looking T errainA voidance(FL T A).
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 foundonMFDHT A WSPageandcharts.
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.
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 VIEWturnedon.
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.
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.
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.
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.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 394 ADDITIONAL FEA TURES TheSafeT axidatabasecyclenumbershowninthegure,10S5,isdeciphered.
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.
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.
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 .
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 398 ADDITIONAL FEA TURES Whena chartis notavailable byselecting the SHW CHR T Softkeyor .
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.
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 Softkeyr etur ns tothe airportdiagram chartwhen theview ison aterminal procedur e chart.
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 CharlotteClassBAirspaceChart(Figure8-27).
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 402 ADDITIONAL FEA TURES Selecting the ST AR SoftkeydisplaystheStandardT erminalArrivalChartifavailable.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 403 ADDITIONAL FEA TURES Selecting the WX Softkeyshows theairportweatherfrequencyinformation, andincludesweatherdata such as MET AR and T AF from the XM Data Link Receiver , when available.
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 Ai.
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 Softkeydisplaysthenextlevelofsoftkeys,thechartoptionslevel(Figure8-20). Selecting the ALL Softkeyshowsthecompleteapproachchartonthescr een.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 406 ADDITIONAL FEA TURES Selecting the HEADER Softkeyshowstheheaderview(approachchartbriengstrip)onthescr een.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 407 ADDITIONAL FEA TURES Selecting the PROFILE Softkeydisplaystheapproachchartdescentpr olestrip.
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 changesthechartsizetottheavailablescreenwidth.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 409 ADDITIONAL FEA TURES Selecting the FULL SCN Softkeyalternatesbetweenremovingandreplacingthedatawindowtotheright.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 410 ADDITIONAL FEA TURES Thefullscreenviewcanalsobeselectedbyusingthepagemenuoption. Selecting full screen On or Off: 1) While viewing a terminal chart press the MENU K ey to display the P age Menu OPTIONS .
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 411 ADDITIONAL FEA TURES D A Y/NIGHT VIEW ChartViewcan bedisplayed ona whiteor black backgr ound for dayor nightviewing. TheDay V iew offers abetter presentation ina brightenvironment.
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 ™ 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 ChartViewdatabaseisr evisedevery14days.
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.
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.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 416 ADDITIONAL FEA TURES 8.4 FLITECHARTS FliteChartsis anoptional featurer esemblingthepaper versionof AeroNav Servicesterminal procedures charts.
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 .
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 418 ADDITIONAL FEA TURES Whena chartis notavailable byselecting the SHW CHR T Softkeyor .
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.
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 Softkeyr etur ns tothe airportdiagram chartwhen theview ison aterminal procedur e chart.
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 AKEOFF MINIMUMSis selected. Pressing the ENT Key displaysthe T ake-offMinimumsandDeparturePr oceduresChart(Figure8-55).
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 422 ADDITIONAL FEA TURES Selecting the ST AR SoftkeydisplaystheStandardT erminalArrivalChartifavailable. Figure 8-57 Arrival Information P age Selecting the APR Softkeydisplaystheapproachchartfortheairportifavailable.
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 weatherdatasuchasMET ARandT AFfromtheXMDataLinkReceiver .
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 Softkeydisplaysthenextlevelofsoftkeys,thechartoptionslevel(Figure8-48). Selecting the ALL Softkeyshowsthecompletechartonthescreen.
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.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 426 ADDITIONAL FEA TURES Selecting the FULL SCN Softkeyalternatesbetweenremovingandreplacingthedatawindowtotheright.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 427 ADDITIONAL FEA TURES Thefullscreenviewcanalsobeselectedbyusingthepagemenuoption. Selecting full screen On or Off: 1) While viewing a terminal chart press the MENU K ey to display the P age Menu OPTIONS .
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 428 ADDITIONAL FEA TURES D A Y/NIGHT VIEW FliteChartscan bedisplayedon awhiteor blackbackgroundfordayor nightviewing. TheDay V iew of fers abetter presentation ina brightenvironment.
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 .
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.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 431 ADDITIONAL FEA TURES Whenthe 180daygrace periodhas expired,‘Chartdata isdisabled.’in yellowindicates thattheFliteCharts database has expired and is no longer viewable.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 432 ADDITIONAL FEA TURES The FliteChartsdatabase is providedfromGarmin. Refer toUpdating Garmin Databases inAppendixB for instructionsonrevisingtheFliteChartsdatabase.
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).
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 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 andExpir esdate ofthe databasecycle canalso be found on the AUX-SystemStatuspage,asseeninFigure8-72.
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 .
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.
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 .
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 439 ADDITIONAL FEA TURES DISABLE/ENABLE IRIDIUM TRANSCEIVER Iridiumtelephoneanddatacommunicationsmaybeturnedonoroffbyperformingthesesimplesteps.
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.
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 .
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.
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’.
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.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 445 ADDITIONAL FEA TURES When thephone is answered,the connectionis established as shownin Figure 8-84. T oexit the call, select the HANGUP Softkey .
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’.
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.
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.
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 Thepop-upalertsmaybeenabledordisabledthroughthePageMenu.
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 Afterreadingatextmessage,areplymaybesent. Replying to a text message: While viewing the text message , select the REPL Y Softk ey .
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 .
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.
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.
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 .
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 .
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 456 ADDITIONAL FEA TURES MANA GING TEXT MESSAGES The viewedmessages maybe listed according tothe date/timethe message wassent orr eceived,the type of message(read,unread,sent,unsent,etc.
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.
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’.
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.
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.
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’.
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.
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.
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 .
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.
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 .
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 .
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.
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 CHANN.
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.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 471 ADDITIONAL FEA TURES PRESETS Up to15 channelsfr omany categor y canbe assigneda presetnumber . The preset channelsare selectedby selecting the PRESETS and MORE Softkeys.
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 usedto enter and display reminder messages (e.
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.
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.
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.
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.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 477 ADDITIONAL FEA TURES INPUT SELECTION Whileonthe AUX-VIDEOPage,pressthe INPUT SoftkeytoselectInput1 orInput2.The selectedinput isdisplayedintheupperleftofthevideodisplay .
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 trafc inputs.
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.
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 Somequicktroubleshootingstepslistedbelowcanbeperformedtondthepossiblecauseofafailur e.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 481 ADDITIONAL FEA TURES Ifafailurestillexists,thefollowingmessagesmaypr ovideinsightasto.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B 482 ADDITIONAL FEA TURES B lank P age.
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.
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 .
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 .
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 Int.
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 .
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 .
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 err.
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.
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 .
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.
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.
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.
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 .
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 .
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 .
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 .
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 .
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 .
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.
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.
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 .
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 .
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.
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.
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).
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 i.
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 .
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.
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.
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 .
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 En.
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 Navi.
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.
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.
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 .
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.
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 • ManualcoursechangeonHSI.
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 adeparture is activated, theCourse DeviationIndicator (CDI) full scaledeection isset to 0.
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.
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 .
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-towe.
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.
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 G.
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 e.
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 to.
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 528 APPENDIX F B lank P age.
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 ------------------------.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B I-2 INDEX Datalink receiver troubleshooting ----------------------- 480 Data report------------------------------------------.
190-01255-00 Rev . B Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX I-3 INDEX Indicated Altitude ------------------------------------------ 248 Initialization (system) -------------------------.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B I-4 INDEX Reduced Protection Mode -------------------------------- 346 Register ---------------------------------------------.
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) -------------.
Garmin G1000H ™ Pilot’ s Guide for the Bell 407GX 190-01255-00 Rev . B I-6 INDEX B lank P age.
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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 .
Ein wichtiger Punkt beim Kauf des Geräts Garmin G1000H (oder sogar vor seinem Kauf) ist das durchlesen seiner Bedienungsanleitung. Dies sollten wir wegen ein paar einfacher Gründe machen:
Wenn Sie Garmin G1000H noch nicht gekauft haben, ist jetzt ein guter Moment, um sich mit den grundliegenden Daten des Produkts bekannt zu machen. Schauen Sie zuerst die ersten Seiten der Anleitung durch, die Sie oben finden. Dort finden Sie die wichtigsten technischen Daten für Garmin G1000H - auf diese Weise prüfen Sie, ob das Gerät Ihren Wünschen entspricht. Wenn Sie tiefer in die Benutzeranleitung von Garmin G1000H reinschauen, lernen Sie alle zugänglichen Produktfunktionen kennen, sowie erhalten Informationen über die Nutzung. Die Informationen, die Sie über Garmin G1000H erhalten, werden Ihnen bestimmt bei der Kaufentscheidung helfen.
Wenn Sie aber schon Garmin G1000H besitzen, und noch keine Gelegenheit dazu hatten, die Bedienungsanleitung zu lesen, sollten Sie es aufgrund der oben beschriebenen Gründe machen. Sie erfahren dann, ob Sie die zugänglichen Funktionen richtig genutzt haben, aber auch, ob Sie keine Fehler begangen haben, die den Nutzungszeitraum von Garmin G1000H verkürzen könnten.
Jedoch ist die eine der wichtigsten Rollen, die eine Bedienungsanleitung für den Nutzer spielt, die Hilfe bei der Lösung von Problemen mit Garmin G1000H. Sie finden dort fast immer Troubleshooting, also die am häufigsten auftauchenden Störungen und Mängel bei Garmin G1000H gemeinsam mit Hinweisen bezüglich der Arten ihrer Lösung. Sogar wenn es Ihnen nicht gelingen sollte das Problem alleine zu bewältigen, die Anleitung zeigt Ihnen die weitere Vorgehensweise – den Kontakt zur Kundenberatung oder dem naheliegenden Service.
