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Garmin G1000:Socata, Pilot'S Manual


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190-00709-00  Rev. A

Garmin G1000 Pilot’s Guide for the Socata TBM 850

6-43

HAZARD AVOIDANCE

Adjusting antenna tilt on the Vertical Scan display:

1) 

Select the

 TILT

 Softkey to activate the cursor in the TILT field and display the Tilt Line.

 

If the Tilt Line is not displayed, press the 

MENU

 Key and turn the large

 FMS

 Knob to select Show Tilt Line.  Press 

the 

ENT

 Key.

2) 

Turn the small

 FMS

 Knob to adjust the antenna tilt angle.  The selected tilt angle is implemented when Horizontal 

Scan is again selected.

The 

RANGE

 Knob

 can also be used to adjust tilt.

Figure 6-49  Adjusting Tilt on Vertical Scan Display

Scan Line

Tilt Line

Summary of Contents for G1000:Socata

Page 1: ...Socata TBM 850...

Page 2: ...isseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin hereby grants permission to download a single copy of this manual and of...

Page 3: ...SING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE STATUTORY OR OTHERWISE THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS WHICH MAY VARY FROM STATE TO STATE IN NO EVENT SHALL...

Page 4: ...ulated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary signi cantly from the altitude displayed by pressure altimeters such as the GDC 74A Air Data Computer or other alt...

Page 5: ...cleaner that is speci ed as safe for anti re ective coatings NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and...

Page 6: ...rmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 00 Rev A iv REVISION INFORMATION Record of Revisions Part Number Revision Date Page Range Description 190 00709 00 A 11 2 07 All Initial Relea...

Page 7: ...nnunciations and Alerting Functions 2 30 System Alerting 2 30 Traf c Annunciation 2 31 TAWS Annunciations 2 31 Altitude Alerting 2 32 Low Altitude Annunciation 2 32 Minimum Descent Altitude Decision H...

Page 8: ...Airports 5 31 Intersections 5 37 NDBs 5 39 VORs 5 41 User Waypoints 5 43 5 4 Airspaces 5 48 5 5 Direct to Navigation 5 53 5 6 Flight Planning 5 59 Flight Plan Creation 5 60 Adding Waypoints To An Exis...

Page 9: ...7 4 Lateral Modes 7 23 Roll Hold Mode ROL 7 24 Low Bank Mode 7 24 Heading Select Mode HDG 7 25 Navigation Mode GPS VOR LOC 7 26 Approach Mode GPS VAPP LOC 7 28 Backcourse Mode BC 7 30 7 5 Autopilot a...

Page 10: ...OF CONTENTS G1000 System Annunciations A 4 G1000 System Message Advisories A 7 AFCS Alerts A 19 TAWS ALERTS A 20 Other G1000 Aural Alerts A 21 SD Card Use B 1 Jeppesen Databases B 1 Garmin Databases...

Page 11: ...egrated Avionics Unit GDC 74B Air Data Computer ADC GEA 71 Engine Airframe Unit GRS 77 Attitude and Heading Reference System AHRS GMU 44 Magnetometer GMA 1347D Cabin Dual Audio System with Integrated...

Page 12: ...and with the on side GIA 63W Integrated Avionics Unit through a High Speed Data Bus HSDB connection GDU 1500 Features a 15 inch LCD with 1024 x 768 resolution and is con gured as an MFD This unit is...

Page 13: ...engine and airframe sensors This unit communicates with both GIA 63Ws using an RS 485 digital interface GRS 77 Provides aircraft attitude and heading information via ARINC 429 to both the on side GDU...

Page 14: ...3D includes Mode S with diversity and is indicated as XPDR1 The GTX 33 is indicated as XPDR2 Both transponders can be controlled from either PFD and only one transponder can be active at a time Each t...

Page 15: ...The GSA 81 servos are used for the automatic control of roll yaw pitch and pitch trim These units interface with each GIA 63W The GSM 85 servo gearbox is responsible for transferring the output torqu...

Page 16: ...IA 63W 1 GMC 710 GMU 44 1 GEA 71 2 GEA 71 1 GDC 74B 1 OAT Probe GMA 1347D Cabin 2 GMA 1347D Cabin 1 GTX 33D GTX 33 GCU 475 GWX 68 GDL 69A GRS 77 2 GMU 44 2 GDC 74B 2 OAT Probe VHF COM VHF NAV LOC GPS...

Page 17: ...ols GMC 710 are described in the CNS Audio Panel and AFCS sections respectively The G1000 system controls are located on the PFD and MFD bezels MFD Control Unit AFCS Control Unit and audio panel The c...

Page 18: ...ency eld as a percentage Press to turn the COM automatic squelch ON and OFF 9 Direct to Key Allows the user to enter a destination waypoint and establish a direct course to the selected destination th...

Page 19: ...ered in the applicable window by turning the small and large knobs In this case the large knob moves the cursor on the page while the small knob selects individual characters for the highlighted curso...

Page 20: ...s or con rms a menu selection or data entry 12 CLR Key Erases information cancels entries or removes page menus Pressing and holding this key displays the Navigation Map Page automatically 13 SPC Key...

Page 21: ...rence for the Pitch Vertical Speed and Flight Level Change modes 12 VNV Key Selects deselects Vertical Navigation mode 13 ALT SEL Knob Sets the selected altitude in the Selected Altitude Box In additi...

Page 22: ...selected when this key is pressed allowing received audio from the the 1 Com receiver to be heard COM2 receiver audio can be added by pressing the COM2 Key 2 COM1 When selected audio from the 1 Com re...

Page 23: ...or off the audio from the ADF receiver 16 NAV2 When selected audio from the 2 Nav receiver can be heard 17 AUX Not used on some aircraft 18 MAN SQ Pressing activates deactivates intercom manual squelc...

Page 24: ...quipped with two SD card slots SD cards are used for aviation database and system software updates as well as terrain database storage To install an SD card Insert the SD card in the SD card slot push...

Page 25: ...wer up Upon power up key annunciator lights also become momentarily illuminated on the audio panels the control units and the display bezels On the PFD the AHRS begins to initialize and displays AHRS...

Page 26: ...COM and NAV frequency selection MFD In normal mode the right portion of the MFD displays a full color moving map with navigation information while the left portion of the MFD is dedicated to the Engin...

Page 27: ...as follows PFD1 By pressing the DISPLAY BACKUP button on the left audio panel MFD By pressing the DISPLAY BACKUP button on the left or the right audio panel PFD2 By pressing the DISPLAY BACKUP button...

Page 28: ...Mode Heading Invalid available available unavailable u n a v a i l a b l e available unavailable unavailable available Air Data Magnetometer Data unavailable available GPS Data Magnetometer Data Air...

Page 29: ...unciations and alerts refer to Appendix A Refer to the Airplane Flight Manual AFM for additional information regarding pilot responses to these annunciations When an LRU or an LRU function fails a lar...

Page 30: ...kground and automatically switch back to white text on black background when selected If messages remain after acknowledgement the MSG Softkey is black on white The PFD softkeys provide control over i...

Page 31: ...DF frequency HSI FRMT Provides access to the HSI formatting softkeys 360 HSI Displays the HSI in a 360 degree view ARC HSI Displays the HSI as an arc BRG2 Cycles the Bearing 2 Information Window throu...

Page 32: ...t acquisition squit ter and replies to discretely addressed Mode S interrogations VFR Automatically enters the VFR code 1200 in the U S A only CODE Displays transponder code selection softkeys 0 7 0 7...

Page 33: ...he top level softkeys BACK MSG ADC2 ADC1 AHRS1 AHRS2 Figure 1 19 PFD Con guration Softkeys Select the BACK Softkey to return to the top level softkeys ALTUNIT METERS IN HPA HSI FRMT 360 HSI ARC HSI Fi...

Page 34: ...cal data e g coastlines terrain rivers lakes and elevation scale on Navigation Map TERRAIN Displays terrain information on Navigation Map AIRWAYS Displays airways on the map cycles through the followi...

Page 35: ...H ON GPS 1 or BOTH ON GPS 2 are then displayed in the Reversionary Sensor Window see Appendix A indicating which GPS receiver is being used Both GPS receivers are still functioning properly but one re...

Page 36: ...IM Softkey Selected SBAS Softkey Selected GPS Selection Softkeys The GPS Status Page provides the following information Satellite constellation diagram Satellites currently in view are shown at their...

Page 37: ...PS solution 3D NAV is indicated as the solution until the 3D differential x has nished acquisition SBAS Satellite Based Augmentation System indicates INACTIVE When acquisition is complete the solution...

Page 38: ...COMPUTE RAIM RAIM has not been computed for the current waypoint time and date combination COMPUTING AVAILABILITY RAIM calculation in progress RAIM AVAILABLE RAIM is predicted to be available for the...

Page 39: ...the necessary data and the satellite signal can be used Green bar Satellite is being used for the GPS solution Checkered bar Receiver has excluded the satellite Fault Detection and Exclusion D indica...

Page 40: ...active page title box are displayed in the upper right of the screen MFD Figure 1 24 Page Title Page Group Active Page Title Figure 1 25 Page Group Icons Page Groups Selected Page Pages in Current Gro...

Page 41: ...selected screen until a different screen softkey is pressed Figure 1 26 Map Pages Map Pages MAP Navigation Map Traf c Map Stormscope Weather Radar Weather Data Link service optional Terrain Figure 1...

Page 42: ...Weight Planning Trip Planning Utility GPS Status System Setup XM Satellite screens XM Information INFO softkey XM Radio RADIO softkey System Status XM Satellite Screens Figure 1 29 Nearest Pages Neare...

Page 43: ...any time on the MFD by pressing the PROC Key A menu is initialized and when a departure approach or arrival is selected the appropriate Procedure Loading Page is opened Turning the FMS Knob does not...

Page 44: ...on MFD Data Bar elds GPS Course Deviation Indicator CDI range COM transceiver channel spacing Displayed nearest airports Figure 1 32 System Setup Page MFD Data Bar Fields Box GPS CDI Box COM Con gurat...

Page 45: ...atus Box When set to AUTO magnetic variation is gured into the displayed value When TRUE is selected no magnetic variation is calculated and a T is displayed next to the value Distance and speed metri...

Page 46: ...ts for the following airspaces can be turned on off in the Airspace Alerts Box Class B TMA Class C TCA Class D Restricted MOA Military Other airspaces An altitude buffer is also provided which expands...

Page 47: ...FMS Knob to display and scroll through the data options list and press the ENT Key when the desired data selection is highlighted The following data may be selected for display in each of the four el...

Page 48: ...ion Box on the System Setup Page allows the pilot to select 8 33 kHz or 25 0 kHz COM frequency channel spacing To change COM channel spacing 1 While on the System Setup Page press the FMS Knob momenta...

Page 49: ...a pilot pro le When the system is powered on the last selected pilot pro le is shown on the MFD Power up Splash Screen Figure 1 8 The G1000 can store up to 25 pro les the currently active pro le the a...

Page 50: ...ist and highlight the desired pro le 5 Press the ENT Key The G1000 loads and displays the system settings for the selected pro le Renaming a pro le 1 Use the FMS Knob to select the AUX System Setup Pa...

Page 51: ...mationonallsystemdatabasesisalsodisplayed ActiveLRUsareindicatedbygreencheckmarks and failed LRUs are indicated by red X s Failed LRUs should be noted and a service center informed Figure 1 34 Example...

Page 52: ...to adjust backlighting Refer to the AFM for details NOTE In normal mode backlighting can only be adjusted from PFD1 or PFD2 In reversionary mode it can also be adjusted from the MFD NOTE No other win...

Page 53: ...l FMS Knob in the direction of the green arrowhead to display PFD1 KEY 3 Turn the large FMS Knob to highlight AUTO and turn the small FMS Knob to display the selection box 4 Turn the FMS Knob to selec...

Page 54: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 00 Rev A 1 44 SYSTEM OVERVIEW BLANK PAGE...

Page 55: ...rtical speed and course deviation information In addition to the ight instruments navigation communication terrain traf c and weather information are also presented on the PFDs and are explained in ot...

Page 56: ...ation Indicator CDI 7 Horizontal Situation Indicator HSI 8 Outside Air Temperature OAT 9 Softkeys 10 System Time 11 Transponder Status Box 12 Selected Heading Bug 13 Turn Rate Indicator 14 Barometric...

Page 57: ...Vspeed Reference 3 Radar Height 4 Selected Heading 5 Wind Data 6 Inset Map 7 DME Information Window 8 Bearing Information Windows 9 Flight Plan Window 10 Minimum Descent Altitude Decision Height 11 S...

Page 58: ...rspeed VMO at which point it turns red Figure 2 4 Red Pointer Showing Overspeed Actual Airspeed True Airspeed Speed Ranges Airspeed Trend Vector Vspeed References Figure 2 3 Airspeed Indicator A color...

Page 59: ...kt increments when a speed has been changed from a default value an asterisk appears next to the speed 4 Press the ENT Key or turn the large FMS Knob to highlight the ON OFF eld 5 Turn the small FMS K...

Page 60: ...ls are shown for every 10 up to 80 Minor pitch marks are shown for intervening 5 increments up to 25 below and 45 above the horizon line Between 20 below to 20 above the horizon line minor pitch marks...

Page 61: ...the cross pointer format Command Bars is shown in Figure 2 11 Changing Command Bar and Aircraft Symbol format 1 Use the FMS Knob to select the AUX System Setup Page on the MFD 2 Press the FMS Knob to...

Page 62: ...responding to this altitude is shown on the tape if the Selected Altitude exceeds the range shown on the tape the bug appears at the corresponding edge of the tape See the AFCS Section for more inform...

Page 63: ...n Hg or hectopascals hPa when metric units are selected Adjusting the altimeter barometric setting creates discontinuities in VNV vertical deviation moving the descent path For large adjustments it ma...

Page 64: ...using the FMS Knob 2 Press the FMS Knob to activate the cursor Time Format is highlighted 3 Turn the large FMS Knob to highlight the Baro Sync ON OFF eld 4 Turn the small FMS Knob clockwise to ON or...

Page 65: ...When the radar height the aircraft altitude above ground level detected by the radar altimeter is between 40 and 2500 feet the current value is displayed in green above the current aircraft heading F...

Page 66: ...rtical speed with numeric labels and tick marks at 2000 and 4000 fpm in each direction on the non moving tape Minor tick marks are at intervals of 1000 fpm The current vertical speed is displayed in t...

Page 67: ...he Altimeter whenever an ILS frequency is tuned in the active NAV eld A green diamond acts as the Glideslope Indicator like a glideslope needle on a conventional indicator If a localizer frequency is...

Page 68: ...mat 1 Press the PFD Softkey 2 Press the HSI FRMT Softkey 3 Press the 360 HSI or ARC HSI Softkey The 360 HSI Figure 2 23 contains a Course Deviation Indicator CDI with a Course Pointer To From Indicato...

Page 69: ...eing adjusted The light blue bug on the compass rose corresponds to the Selected Heading While the HSI is displayed as an arc if the Selected Heading Bug is adjusted off the shown portion of the compa...

Page 70: ...he navigation angle setting to True at the appropriate time Figure 2 26 Heading and Course Indications True Changing the navigation angle setting 1 Use the FMS Knob to select the AUX System Setup Page...

Page 71: ...igure 2 28 Turn Rate Indicator and Trend Vector BEARING POINTERS AND INFORMATION WINDOWS NOTE When the Arc HSI is displayed the Bearing Information windows and pointers are disabled Two bearing pointe...

Page 72: ...is displayed in the information window if The NAV radio is not receiving the tuned VOR station GPS is the bearing source and an active waypoint is not selected Selecting bearing display and changing...

Page 73: ...Deviation Indicator Flight Phase Scale Crosstrack Error Navigation Source CDI 360 HSI Navigation Source Flight Phase Scale CDI Arc HSI The CDI can display two sources of navigation GPS or NAV VOR loca...

Page 74: ...2 Selected for Tuning VOR2 Selected The system automatically switches from GPS to LOC navigation source and changes the CDI scaling accordingly when all of the following occur A localizer or ILS appro...

Page 75: ...Is are synchronized CDI SYNC turned on they remain synchronized for the entire ight Synchronizing the CDIs 1 Select the AUX System Setup Page using the FMS Knob 2 Press the FMS Knob to activate the cu...

Page 76: ...g may also be changed 2 0 nm 1 0 nm 0 3 nm or Auto from this page If the selected scaling is smaller than the automatic setting for enroute and terminal phases the CDI is scaled accordingly and the se...

Page 77: ...om the departure airport or the leg after the last departure waypoint has been activated or a direct to waypoint is activated If after completing the departure procedure the nearest airport is more th...

Page 78: ...owing conditions The next leg in the missed approach procedure is not aligned with the nal approach path The next leg in the missed approach procedure is not a CA CD CF CI CR DF FA FC FD FM IF or TF A...

Page 79: ...ired the course to from the waypoint can now be adjusted When OBS Mode is disabled the GPS ight plan returns to normal operation with automatic sequencing of waypoints following the course set in OBS...

Page 80: ...pproach point MAP automatic approach waypoint sequencing is suspended SUSP appears on the HSI to the lower right of the aircraft symbol in place of OBS and the OBS Softkey label changes to SUSP SUSP A...

Page 81: ...isplay In addition to the ight instruments the PFD also displays various supplemental information including temperatures wind data and Vertical Navigation VNV indications TEMPERATURE DISPLAYS The Outs...

Page 82: ...WIND DATA Wind data can be displayed in three different ways Figure 2 41 Wind Data No Data Option 2 Option 1 Option 3 Displaying wind data 1 Press the PFD Softkey 2 Press the WIND Softkey to display w...

Page 83: ...ssage Figure 2 42 Vertical Navigation Indications PFD Criteria VNV Indication Removed Required Vertical Speed RVSI Vertical Deviation VDI VNV Target Altitude Aircraft 1 min before the next TOD and not...

Page 84: ...ashing again Pressing the MSG Softkey while the System Messages Window is open closes the window Critical values generated by redundant sensors are monitored by comparators If differences in the sens...

Page 85: ...displaying traf c A ashing black on yellow TRAFFIC annunciation Figure 2 44 appears to the top left of the Attitude Indicator for 5 seconds and remains displayed until no TAs are detected in the area...

Page 86: ...ext on a black background and ashes for 5 seconds After reaching the Selected Altitude if the aircraft ies outside the deviation band 200 feet of the Selected Altitude the Selected Altitude Box change...

Page 87: ...mums is generated When the radar altimeter is selected as the altitude source for the Minimum Descent Altitude alerting function the color of the current radar height changes to yellow Figure 2 48 Bar...

Page 88: ...nnunciations are displayed on the PFD to the left of the Selected Altitude Outer marker reception is indicated in blue middle in amber and inner in white Refer to the Audio Panel and CNS Section for m...

Page 89: ...osition errors INTEG OK Lower left of aircraft symbol Integrity OK GPS integrity has been restored to within normal limits annunciation displayed for 5 seconds DR Upper right of aircraft symbol DeadRe...

Page 90: ...e Bearing Information Alerts and Annunciation windows can be displayed during such situations The following information is removed from the PFD and corresponding softkeys are disabled when the aircraf...

Page 91: ...ation on the left side of the Multi Function Display MFD Synoptics pages are provided for monitoring the status of the doors pressurization electrical fuel and de icing systems The Crew Alerting Syste...

Page 92: ...play PFD symbology together with engine and CAS information refer to the System Overview for more information about Reversionary Mode In Reversionary Mode engine pressurization fuel electrical and tri...

Page 93: ...Speed 4 Interturbine Temperature 5 Oil Pressure 6 Oil Temperature 7 CAS Display 8 Cabin Pressure Altitude and Change Rate 9 Differential Pressure 10 Selected Cabin Altitude 11 Oxygen Pressure 12 Fuel...

Page 94: ...refer to each display description for details If the sensor data for a parameter becomes invalid or unavailable a red X is displayed across the indicator and or readout ENGINE PARAMETERS The TBM 850...

Page 95: ...tarts running When the engine is not running OFF is annunciated above the ITT readout this changes to STRT upon engine start No annunciation is shown when the engine is running normally Figure 3 8 Int...

Page 96: ...si is indicated on a color coded scale with a readout Selected Cabin Altitude is displayed as a digital readout in 100 ft increments with a range from 1 000 to 11 000 feet Figure 3 10 Cabin Pressure D...

Page 97: ...Essential Bus Voltage Battery Voltage Battery Current Figure 3 12 Electrical Display TRIM AND FLAP INDICATORS Elevator rudder and aileron trim indications are shown along slide bar scales next to the...

Page 98: ...em Fuel system Anti ice system Doors Once the SYSTEM Softkey is selected the Synoptics pages can be accessed using softkeys or the small FMS Knob To return to the previously displayed page when a Syno...

Page 99: ...tem to display the system status The generators ground power supply GPU batteries and buses are shown in green to denote normal operation Color of the units change depending on the condition Figure 3...

Page 100: ...ected the status is shown in gray with the switch closed A CAS message GPU DOOR is generated if the GPU door is open Battery connection status to the main bus is indicated in green direction of curren...

Page 101: ...7 Fuel Synoptics Page 5 4 8 7 1 2 3 6 1 Left Fuel Tank 2 Left Fuel Line 3 Fuel Pressure 4 Auxiliary Boost Pump 5 Fuel Selector 6 Right Fuel Tank 7 Right Fuel Line 8 Fuel Flow Data Status of the fuel s...

Page 102: ...X Weight Planning Page see the Flight Management Section A red X over a component indicated invalid data or a failed unit GENERAL SYSTEMS The General Synoptics Page aircraft diagram displays open door...

Page 103: ...is located in the lower left corner of the EICAS Display on the MFD under normal display conditions Up to 14 messages can be displayed when more than 14 messages accumulate the scrolling CAS softkeys...

Page 104: ...riggered When a new red CAS warning message appears it ashes inversely red on white in conjunction with the Master Warning Indicator Pressing the Master Warning Indicator acknowledges all ashing red m...

Page 105: ...e than 15 USGAL for 30 seconds FUEL LOW L R Fuel quantity less than or equal to 9 1 USG in speci ed tank GPU DOOR GPU receptacle door not closed X X IGNITION Ignition exciter running INERT SEP FAIL In...

Page 106: ...t transitions from on ground to in air Table 3 5 Takeoff Operation Phase Inhibit TOPI Activation Deactivation Criteria Activation Deactivation Transitions from in air to on ground On ground 25 sec IAS...

Page 107: ...Q When no audio is detected MASQ processing further reduces the amount of background noise from the radios The Mode S Transponders are controlled with softkeys and the FMS Knob located on the Primary...

Page 108: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 4 2 AUDIO PANEL AND CNS PFD CONTROLS AND FREQUENCY DISPLAY Figure 4 1 PFD Controls COM NAV Frequency Tuning Boxes and ADF DME Tuning Window 12 2 1 6...

Page 109: ...ght blue box and Frequency Transfer Arrow between COM1 and COM2 7 COM Frequency Transfer Key Transfers the standby and active COM frequencies Press and hold this key for two seconds to tune the emerge...

Page 110: ...is simultaneously selected when this key is pressed allowing received audio from the 1 COM receiver to be heard COM2 receive can be added by pressing the COM2 Key 2 COM1 When selected audio from the...

Page 111: ...l ADF receiver audio on or off 16 NAV2 When selected audio from the 2 NAV receiver can be heard 17 AUX Not used in the TBM 850 18 MAN SQ Enables manual squelch for the intercom When the intercom is ac...

Page 112: ...t The COM transceiver is selected for transmitting by pressing the COM MIC Keys on the Audio Panel During reception of audio from the COM radio selected for transmission audio from the other COM radio...

Page 113: ...ected on both Audio Panels the pilot has transmit priority on COM1 the copilot has transmit priority on COM2 COM TRANSCEIVER MANUAL TUNING The COM frequency controls and frequency boxes are on the rig...

Page 114: ...xes Press the COM Knob to Switch the Tuning Box From One COM Radio to the Other QUICK TUNING AND ACTIVATING 121 500 MHZ Pressing and holding the COM Frequency Transfer Key for two seconds automaticall...

Page 115: ...y is entered it becomes a standby frequency Pressing the Frequency Transfer Key places this frequency into the COM Active Frequency Field Auto tuning a COM frequency for a nearby airport from the PFD...

Page 116: ...M frequency can be auto tuned activate the cursor by pressing the GCU 475 FMS Knob or selecting the appropriate softkey 2 Turn the FMS Knob to place the cursor on the desired COM frequency Figure 4 11...

Page 117: ...nu options 3 Press the ENT Key to place the cursor on the desired selection 4 Scroll through the frequency selections with the FMS Knob or the ENT Key 5 Press the ENT Key to load the COM frequency int...

Page 118: ...g the FMS Knob and scrolling through the list The frequency is transferred to the COM Standby Field with the ENT Key Press ENT Key to load frequency into PFD1 COM Standby Field Cursor then advances to...

Page 119: ...s can also be auto tuned from the NRST Nearest Airspaces NRST Nearest Frequencies and NRST Nearest Airports Pages on the MFD in a similar manner using the appropriate softkeys or MENU Key the FMS Knob...

Page 120: ...e System Setup Page of the AUX Page Group Figure 4 13 COM Channel Spacing 25 kHz Channel Spacing 8 33 kHz Channel Spacing Changing COM frequency channel spacing 1 Select the AUX System Setup Page 2 Pr...

Page 121: ...nob again enables Automatic Squelch When Automatic Squelch is disabled a white SQ appears next to the COM frequency Figure 4 15 Overriding Automatic Squelch Squelch Indication Press the COM VOL SQ Kno...

Page 122: ...d the Frequency Transfer Arrow are placed in the active NAV Frequency Field and the active NAV frequency color changes to green The three navigation modes that can be cycled through are VOR1 or LOC1 I...

Page 123: ...he NAV frequency controls and frequency boxes are on the left side of the PFDs Manually tuning a NAV frequency 1 Turn the NAV Knob to tune the desired frequency in the NAV Tuning Box 2 Press the Frequ...

Page 124: ...he NAV1 or NAV2 Key on the Audio Panel Pressing the VOL ID Knob turns off the Morse code audio only in the radio with the NAV Tuning Box To turn off both NAV IDs transfer the NAV Tuning Box between NA...

Page 125: ...quency Box from pages in the NRST or WPT page group by highlighting the frequency and pressing the ENT Key Figures 4 23 4 24 and 4 25 Auto tuning a NAV frequency from the WPT and NRST Pages 1 From any...

Page 126: ...ll through the menu options 3 Press the ENT Key to place the cursor in the desired window 4 Scroll through the frequency selections with the FMS Knob or the ENT Key 5 Press the ENT Key to load the NAV...

Page 127: ...used to scroll through the list The cursor is placed on the frequency with the FREQ Softkey and loaded into the NAV Tuning Box with the ENT Key Select the FREQ Softkey to Place the Cursor on the VOR...

Page 128: ...auto tuned from the NRST Nearest Airports WPT Airport Information WPT VOR Information and NRST Nearest Frequencies Pages on the MFD in a similar manner using the appropriate softkeys or MENU Key the F...

Page 129: ...tion on both PFD1 and PFD2 When loading or activating a VOR or ILS LOC approach the approach frequency is automatically transferred to a NAV frequency eld as follows If the current CDI navigation sour...

Page 130: ...Muted and Deselected Pressing the MKR MUTE Key selects and deselects marker beacon audio The key annunciator indicates when marker beacon audio is selected During marker beacon audio reception pressi...

Page 131: ...tuned by pairing with a VHF NAV frequency DME frequency pairing is automatic and only the VHF NAV frequency is shown The following ADF DME information is displayed in the ADF DME Tuning Window Active...

Page 132: ...the ENT Key to complete data entry for the standby frequency Figure 4 30 Entering ADF Standby Frequencies Press the ENT Key to Complete ADF Frequency Entry Turn the Small FMS Knob to Enter Data in th...

Page 133: ...equency Oscillator The ADF bearing pointer parks on the HSI at 90 degrees while an audible tone is provided when a signal is received This mode also allows identi cation of the interrupted carrier bea...

Page 134: ...airs the DME frequency from the selected NAV1 frequency NAV2 Pairs the DME frequency from the selected NAV2 frequency HOLD When in the HOLD position the DME frequency remains paired with the last sele...

Page 135: ...voidance System TAS to recognize the presence of Mode S equipped aircraft for selective interrogation The Hazard Avoidance Section provides more details on traf c avoidance systems TRANSPONDER CONTROL...

Page 136: ...ate the other transponder When turning on the G1000 for use the system activates Transponder 1 as the default unit regardless of which transponder was active prior to shutdown When switching between T...

Page 137: ...be returned to Ground Mode by selecting the GND Softkey GND Mode Figure 4 36 Ground Mode STANDBY MODE MANUAL NOTE In Standby Mode the IDENT function is inhibited Standby Mode can be selected at any t...

Page 138: ...de is selected a green ALT indication and transponder code appear in the mode eld of the Transponder Data Box and all transponder replies requesting altitude information are provided with pressure alt...

Page 139: ...the transponder code becomes active Entering a Code Figure 4 41 Entering a Code Entering a transponder code with the PFD FMS Knob 1 Select the XPDR and the CODE Softkeys as in the previous procedure...

Page 140: ...ter for con guration Figure 4 43 VFR Code VFR Code IDENT FUNCTION NOTE In Standby Mode the IDENT Softkey is inoperative Selecting the IDENT Softkey sends an ID indication to Air Traf c Control ATC The...

Page 141: ...y Entering a Flight ID 1 Select the TMR REF Softkey to display the Timer References Window 2 Press the FMS Knob to activate the selection cursor if not already activated 3 Turn the large FMS Knob to s...

Page 142: ...n a monaural headset hears only the left channel in both ears If a monaural headset is used at one of the passenger positions any other passenger using a stereo headset hears audio in the left ear onl...

Page 143: ...m squelch setting Pressing the MAN SQ Key enables manual squelch control indicated by the MAN SQ annunciator During manual squelch operation pressing the ICS Knob toggles between volume and squelch ad...

Page 144: ...dphones When PA is selected on the Audio Panel the annunciator ashes about once per second while pressing the PTT the COM MIC annunciator is no longer lit and the active COM frequency for that Audio P...

Page 145: ...LAY Key controls the play function The PLAY annunciator ashes to indicate when play is in progress The PLAY annunciator turns off after playback is nished Pressing the PLAY Key once plays the latest r...

Page 146: ...olume level The time required for MUSIC 1 volume to return to normal is between one half and four seconds MUSIC 1 MUTING ENABLE DISABLE Pressing and holding the MUSIC Key for three seconds switches MU...

Page 147: ...one another but the radio volumes are not NOTE When the MAN SQ Key is pressed the ICS squelch can be set manually by the pilot and copilot If manual squelch is set to full open SQ annunciated and the...

Page 148: ...pilot or copilot headset Setting the Audio Panels during pre ight 1 Verify that the INTR COM Key is selected 2 Verify that the MAN SQ Annunciator is extinguished 3 Turn the MSTR Knob Master Volume Con...

Page 149: ...mitting after 35 seconds of continuous operation An alert appears on the PFD to advise the crew of a stuck microphone The COM1 MIC or COM2 MIC Key Annunciator on the Audio Panel ashes as long as the P...

Page 150: ...uency is not shown The COM1 emergency frequency is available to both the copilot and pilot Figure 4 54 Frequency Section of PFD2 Display after PFD1 Failure Emergency Channel Loaded Automatically If PF...

Page 151: ...e speakers If there is a failure of one Audio Panel that side only has access to their respective on side fail safe COM If there is a failure of one Audio Panel the remaining one does not have access...

Page 152: ...190 00709 00 Rev A Garmin G1000 Pilot s Guide for the Socata TBM 850 4 46 AUDIO PANEL AND CNS BLANK PAGE...

Page 153: ...e OFF Softkey removes the Inset Map The Navigation Map displays aviation data e g airports VORs airways airspaces geographic data e g cities lake highways borders topographic data map shading indicati...

Page 154: ...Window Procedures Window Nearest Airports Window Inset Map Navigation Status Box Navigation Mode Figure 5 2 GPS Navigation Information on the MFD Navigation Page Active Flight Plan Leg Navigation Map...

Page 155: ...ox located at the top of the MFD contains four data elds each displaying one of the following items Bearing BRG Distance DIS Desired Track DTK Endurance END Enroute Safe Altitude ESA Estimated Time of...

Page 156: ...range Wind direction and speed Map orientation Icons for enabled map features Aircraft icon representing present position Nav range ring Flight plan legs User waypoints Track vector Topography scale T...

Page 157: ...active ight plan legs in a non North Up orientation the map does not show the map orientation nor the wind direction and speed NOTE Map orientation can only be changed on the Navigation Map Page Any...

Page 158: ...RANGE There are 28 different map ranges available from 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...

Page 159: ...Map Group These settings determine the minimum and maximum distance to display based upon the aircraft s ground speed Waypoints that are long distances apart cause the map range to increase to a point...

Page 160: ...isplayed The cursor ashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed 3 Select the Map group 4 Press the ENT Key 5 Highlight the AUTO ZOOM eld 6 Select Off MFD Only PFD...

Page 161: ...cted by pressing the Joystick the Map Pointer ashes on the map display A window also appears at the top of the map display showing the latitude longitude position of the pointer the bearing and distan...

Page 162: ...d 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 dis...

Page 163: ...tion includes the name and class of airspace the ceiling in feet above Mean Sea Level MSL and the oor in feet MSL Figure 5 10 Navigation Map Map Pointer on Airspace Map Pointer on Airspace Information...

Page 164: ...the Map Pointer on a waypoint 2 Press the ENT Key to display the Waypoint Information Page for the selected waypoint 3 Press the GO BACK Softkey the CLR Key or the ENT Key to exit the Waypoint Informa...

Page 165: ...an open area within the boundaries of an airspace 2 Press the ENT Key to display an options menu 3 Review Airspace should already be highlighted if not select it Press the ENT Key to display the Airs...

Page 166: ...navigation map Measuring bearing and distance between any two points 1 Press the MENU Key with the Navigation Map Page displayed 2 Highlight the Measure Bearing Distance eld 3 Press the ENT Key A Meas...

Page 167: ...opographic data on all pages displaying navigation maps 1 Press the MAP Softkey the INSET Softkey for the PFD Inset Map 2 Press the TOPO Softkey 3 Press the TOPO Softkey again to remove topographic da...

Page 168: ...removes the same item at 50 nm Selecting a topographical data range TOPO DATA 1 Press the MENU Key with the Navigation Map Page displayed The cursor ashes on the Map Setup option 2 Press the ENT Key...

Page 169: ...displayed Range of Displayed Elevations Displaying removing the topographic scale TOPO SCALE 1 Press the MENU Key with the Navigation Map Page displayed The cursor ashes on the Map Setup option 2 Pre...

Page 170: ...ng items are con gured on the land menu Land Symbols Text label size can be None Small Medium Med or Large Lrg Symbol Default Range nm Maximum Range nm Latitude Longitude LAT LON Off 2000 Highways and...

Page 171: ...NAVAIDs 2000 2000 Large Airports LARGE APT 250 500 Medium Airports MEDIUM APT 150 300 Small Airports SMALL APT 50 100 Taxiways SAFETAXI See Section 8 3 20 Runway Extension RWY EXTENSION N A Off 100 In...

Page 172: ...ess the FMS Knob to return to the Navigation Map Page Figure 5 18 Navigation Map Setup Menu TOPO SCALE Setup LAND DATA On Off The label size TEXT sets the size at which labels appear on the display no...

Page 173: ...t Label Size Off Small Med or Lrg Figure 5 20 Navigation Map Setup Menu AVIATION GROUP Setup Maximum Display Range Text Label Size Off Small Med or Lrg NOTE Since the PFD Inset Map is much smaller tha...

Page 174: ...tter Level Navigation Map Page Menu DCLTR Softkey Decluttering the map Select the DCLTR Softkey with the Navigation Map Page displayed The current declutter level is shown With each softkey selection...

Page 175: ...national Borders X X X X Track Vector X X X X Navigation Range Ring X X X X Fuel Range Ring X X X X Terrain Data X X X X Traf c X X X X Airways X X X X NEXRAD X X X XM Lightning Data X X X Airports X...

Page 176: ...rways since they run primarily between VORs High Altitude Airways or Jet Routes primarily serve airliners jets turboprops and turbocharged piston aircraft operating above 18 000 feet MSL Jet Routes st...

Page 177: ...ss the ENT Key The Map Setup Menu is displayed 3 Turn the small FMS Knob to select the Airways group and press the ENT Key 4 Turn the large FMS Knob to highlight the AIRWAYS eld 5 Turn the FMS Knob to...

Page 178: ...ft track The track vector look ahead time is selectable 30 sec 60 sec default 2 min 5 min 10 min 20 min and determines the length of the track vector The arrowhead is continuously pointing to the pred...

Page 179: ...a white arrow pointing in the direction in which the wind is moving for wind speeds greater than or equal to 1 kt Figure 5 26 Navigation Map Wind Vector Wind Direction Wind Speed NOTE The wind vector...

Page 180: ...he Nav Range Ring is not displayed on the Waypoint Information pages Nearest pages or Direct to Window map Displaying removing the Nav Range Ring 1 Press the MENU Key with the Navigation Map Page disp...

Page 181: ...Displaying removing the fuel range ring and selecting a fuel range time 1 Press the MENU Key with the Navigation Map Page displayed The cursor ashes on the Map Setup option 2 Press the ENT Key The Ma...

Page 182: ...ection for detailed instructions on entering data in the G1000 As a waypoint identi er facility name or location is entered the G1000 s Spell N Find feature scrolls through the database displaying tho...

Page 183: ...es COM NAV and lighting review runways and review instrument procedures that may be involved in the ight plan See the Audio Panel and CNS Section for more information on loading frequencies auto tunin...

Page 184: ...rt Soft Unknown or Water Runway lighting type No Lights Part Time Full Time Unknown or PCL Freq for pilot controlled lighting COM Availability TX transmit only RX receive only PT part time i additiona...

Page 185: ...n be loaded using the softkeys on the Airport Information Page See the procedures section for details METARs or TAFs applicable to the selected airport can be selected for display see the Hazard Avoid...

Page 186: ...e MFD is rst in the group of NRST pages because of its potential use in the event of an in ight emergency In addition to displaying a map of the currently selected airport and surrounding area the pag...

Page 187: ...r press the CLR Key The cursor is now on the next airport in the nearest airports list Repeatedly pressing the ENT Key moves through the airport list alternating between the Nearest Airports Window an...

Page 188: ...t are not appropriately surfaced from being displayed Default settings are 0 feet or meters for runway length and ANY for runway surface type Selecting nearest airport surface matching criteria 1 Use...

Page 189: ...oxes labeled INTERSECTION INFORMATION and NEAREST VOR Figure 5 36 Intersection Information Page Selected Intersection Navigation Map Showing Selected Intersection Intersection Identi er Nearest VOR In...

Page 190: ...tersection is indicated by a white arrow Up to seventeen intersections are visible at a time If there are more than can be shown the list can be scrolled If there are no items for display text indicat...

Page 191: ...g Distance to Airport NDB Information Type Region Lat Long NDB Frequency NOTE Compass locator LOM a low power low or medium frequency radio beacon installed in conjunction with the instrument landing...

Page 192: ...er indicates the selected NDB Up to seventeen NDBs are visible at a time If there are more than can be shown each list can be scrolled The list only includes waypoints that are within 200nm If there a...

Page 193: ...beled VOR INFORMATION FREQUENCY and NEAREST AIRPORT Figure 5 40 VOR Information Page Selected VOR Navigation Map Showing Selected VOR VOR Identi er Type Facility Name Nearest City Nearest Airport Info...

Page 194: ...ree boxes labeled NEAREST VOR INFORMATION and FREQUENCY The list only includes waypoints that are within 200 nm A white arrow before the VOR identi er indicates the selected VOR Up to seventeen VORs a...

Page 195: ...ap using the Joystick or from the User Waypoint Information Page by referencing a bearing distance from an existing waypoint or bearing from two existing waypoints Once a waypoint has been created it...

Page 196: ...rs 3 Press the ENT Key The current aircraft position is the default location of the new waypoint 4 If desired highlight the Information Box and enter the latitude and longitude for the waypoint or hig...

Page 197: ...ween Review Airspaces or Create User Waypoint or 3 a new waypoint is initiated with the default name being the selected map item 3 Enter a user waypoint name up to six characters 4 Press the ENT Key t...

Page 198: ...ter a waypoint name or select the waypoint in the User Waypoint List then press the ENT Key 2 Press the MENU Key 3 Select Use Present Position 4 Press the ENT Key twice The new waypoint s location is...

Page 199: ...he ENT Key 4 Press the FMS Knob to remove the ashing cursor Or 1 Highlight a User Waypoint in the User Waypoint List or enter a waypoint in the User Waypoint eld 2 Press the MENU Key 3 Select Delete U...

Page 200: ...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 Temporary Flight Restriction TFR Figure 5 45 Air...

Page 201: ...d the aircraft is more than 500 feet above below an airspace an alert message is not generated but if the aircraft is less than 500 feet above below an airspace and projected to enter it the pilot is...

Page 202: ...pace Alerts DFLTS Softkey Airspace Alerts Box Airspace Altitude Buffer Alert On Off Default Settings Shown Map ranges for the airspace boundaries are selected from the Aviation Group in the Map Setup...

Page 203: ...t only if Ahead or Ahead 2nm Airspace Vertical Limits Ceiling Floor Airspace Agency Info Airspace Type Controlling Agency Softkeys Airspace 1 Associated Frequencies Type Availability Info Frequency Ai...

Page 204: ...RSPC Inside airspace The aircraft is inside the special use airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft penetrates the airspace with...

Page 205: ...a new direct to or ight plan or cancelled A vertical navigation VNV direct to creates a descent path and provides guidance to stay on the path from the current altitude to a selected altitude at the...

Page 206: ...s the CLR Key to remove it or turn the large FMS Knob to select the facility name or city eld and turn the small FMS Knob to begin entering a facility name or city If duplicate entries exist for the e...

Page 207: ...ight plan and the AIRWAY list is available only when the active leg is part of an airway 3 Turn the small FMS Knob clockwise to display the NRST RECENT or AIRWAY waypoints 4 Turn the large FMS Knob cl...

Page 208: ...the pointer 2 Move the Joystick to place the pointer at the desired destination location 3 If the pointer is placed on an existing airport NAVAID or user waypoint the waypoint name is highlighted 4 P...

Page 209: ...guidance to stay on the path from the aircraft s current altitude to the altitude of the direct to waypoint The altitude is reached at the waypoint or at the speci ed distance along the ight path if...

Page 210: ...ENT Removing a VNV altitude constraint 1 Press the Direct to Key to display the Direct to Window 2 Press the MENU Key 3 With Clear Vertical Constraints highlighted press the ENT Key Figure 5 52 Direct...

Page 211: ...ture or arrival the G1000 uses the waypoint information from the current database to de ne the waypoints If the database is changed or updated the G1000 automatically updates the information if the pr...

Page 212: ...EATION There are three methods to create or modify a ight plan Active Flight Plan Page on the MFD create modify the active ight plan Active Flight Plan Window on the PFD create modify the active ight...

Page 213: ...int Destination Waypoint Total Flight Plan Distance Enroute Safe Altitude Catalog Contents Used Empty Softkeys Selected Flight Plan Map The active ight plan is listed on the active Flight Plan Page on...

Page 214: ...r Creating a stored ight plan 1 Press the FPL Key 2 Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page 3 Select the NEW Softkey or press the MENU Key highlight Create New Flight...

Page 215: ...re limited to 99 waypoints including waypoints within airways and procedures If the number of waypoints in the ight plan exceeds 99 the message Flight plan is full Remove unnecessary waypoints appears...

Page 216: ...plicates a Duplicate Waypoint Window is displayed Use the FMS Knob to select the correct waypoint Figure 5 58 Duplicate Waypoints Window Adding a waypoint to the active ight plan 1 Press the FPL Key 2...

Page 217: ...not already in the ight plan select the waypoint after the desired airway entry point select the airway and it is added in front of the selected waypoint An airway can only be loaded if there is a way...

Page 218: ...sition 5 Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown rst in the list followed by all altitude airways and then high altitude airwa...

Page 219: ...Airway UR975 in North Africa has more complicated directional restrictions within the list of airway waypoints AMANO VAKOR LIBRO NELDA DIRKA GZO KOSET and SARKI Starting from AMANO the airway can be...

Page 220: ...res from the navigation database into a ight plan The procedures are designed to facilitate routing of traf c leaving an airport departure arriving at an airport arrival and landing at an airport appr...

Page 221: ...Sequence Preview of Selected Departure Loading a departure procedure into a stored ight plan 1 Select a stored ight plan from the Flight Plan Catalog Page 2 Select the EDIT Softkey or press the MENU K...

Page 222: ...irport Selected Departure Departure Transition Points Available Selected Runway Selected Departure End Point Preview of Selected Departure Selected Transition Figure 5 65 Stored Flight Plan Page Depar...

Page 223: ...uence Preview of Selected Arrival Selected Runway Loading an arrival procedure into a stored ight plan 1 Select a stored ight plan from the Flight Plan Catalog Page 2 Select the EDIT Softkey or press...

Page 224: ...the Transition Destination Airport Selected Arrival Transitions Available with DBRY1 Arrival Waypoint Sequence Preview of Selected Arrival Selected Transition Figure 5 68 Stored Flight Plan Page Arriv...

Page 225: ...roaches Available at KCOS Approach Waypoint Sequence Preview of Selected Approach Loading an approach procedure into a stored ight plan 1 Select a stored ight plan from the Flight Plan Catalog Page 2...

Page 226: ...Approach Selected Transition Figure 5 71 Stored Flight Plan Page Approach Inserted Inserted Approach Header Approach Identi er approach airport runway and approach type e g KCOS RNAV 35RGPS LPV FLIGH...

Page 227: ...ght Plan 5 Press the EDIT Softkey to open the Stored Flight Plan Page and view the waypoints in the ight plan 6 Press the FMS Knob to exit the Stored Flight Plan Page Figure 5 72 Stored Flight Plan In...

Page 228: ...the MENU Key highlight Activate Flight Plan and press the ENT Key The Activate Stored Flight Plan window is displayed 4 With OK highlighted select the ENT Key To cancel the request press the CLR Key o...

Page 229: ...e CLR Key or highlight CANCEL and press the ENT Key Deleting all stored ight plans 1 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page 2 Press the MENU Key 3 Highli...

Page 230: ...white header of the airway to be deleted 3 Press the CLR Key The Remove airway name window is displayed 4 With OK highlighted press the ENT Key To cancel the request press the CLR Key or highlight CA...

Page 231: ...s displayed 7 With OK highlighted press the ENT Key To cancel the request press the CLR Key or highlight CANCEL and press the ENT Key Deleting an entire procedure from a stored ight plan 1 Press the F...

Page 232: ...d Flight Plan Page is displayed 5 Turn the large FMS Knob to highlight the comment eld 6 Use the FMS Knobs to edit the comment 7 Press the ENT Key to accept the changes ALONG TRACK OFFSETS A waypoint...

Page 233: ...rack Offset Waypoint and Distance from Flight Plan Waypoint Entering an along track offset distance 1 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD...

Page 234: ...of the course change NOTE Vertical navigation is unavailable while the Parallel Track feature is active Figure 5 74 Active Flight Plan Window Selecting Parallel Track Selecting Parallel Track Active...

Page 235: ...ack Active Parallel Track Waypoints TIFTO p TOP p SLN p HYS p LAA p Activating Parallel Track affects the entire active ight segment e g enroute Parallel Track Original Track If the parallel track pro...

Page 236: ...Active If the offset direction and distance results in an unreasonable route geometry the status indicates that the system is unable to activate the parallel track because of invalid geometry Figure 5...

Page 237: ...igation guidance Activating a ight plan leg 1 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the FMS Knob to activate the cursor not required...

Page 238: ...ect OK 4 Press the ENT Key to invert and activate the active ight plan To cancel press the CLR Key or highlight CANCEL and press the ENT Key Inverting and activating a stored ight plan 1 Press the FPL...

Page 239: ...display the Active Flight Plan Page 2 Press the VIEW Softkey to display the CUM and LEG LEG Softkeys 3 Press the CUM Softkey to view cumulative waypoint distance or press the LEG LEG Softkey to view...

Page 240: ...When airways are collapsed leg to leg computed values such as DIS or ETE shown for the exit waypoint re ects the total of all the legs on the airway that have been hidden in the collapsed display The...

Page 241: ...eference waypoint and creates a new user waypoint along the ight plan at the location closest to a chosen reference waypoint Determining the closest point along the active ight plan to a selected wayp...

Page 242: ...e desired path is de ned by a line joining two waypoints with speci ed altitudes or as a vertical angle from a speci ed waypoint altitude The vertical waypoints are integrated into the active ight pla...

Page 243: ...tical navigation direct to to any waypoint in the active ight plan with an altitude constraint designated for vertical guidance Selecting the VNV Direct to Softkey on the Active Flight Plan Page allow...

Page 244: ...he Active Flight Plan Page on the MFD 2 Press the VNV PROF Softkey or press the MENU Key highlight SelectVNV Pro leWindow and press the ENT Key The cursor is now located in the CURRENT VNV PROFILE box...

Page 245: ...played as blue text up to but not including the FAF The FAF is always a reference only altitude and cannot be designated unless the selected approach does not provide vertical guidance In this case th...

Page 246: ...itude constraint if the selected waypoint is an airport an additional choice is displayed Turn the small FMS Knob to choose MSL or AGL and press the ENT Key to accept the altitude Altitude constraints...

Page 247: ...to published VNV altitude of nnnnnFT con rmation window is displayed 4 Select REVERT and press the ENT Key The altitude is changed to the navigation database value Modifying a system calculated altit...

Page 248: ...mediate waypoints in the original ight plan but keeps the procedure available on the Active Flight Plan Page for quick activation when needed Activating also adds the procedure to the end of the ight...

Page 249: ...50 5 97 FLIGHT MANAGEMENT Figure 5 87 Departure Selection Departure Airport Departure Preview Available Procedure Actions Departure Choices Loaded Procedures Procedure Loading Page Selection Softkeys...

Page 250: ...he available transitions Press the ENT Key to select the transition The cursor moves to the Sequence box The departure is previewed on the map 7 Select the INFO Softkey to return to the Airport Inform...

Page 251: ...points and a runway LOADING AN ARRIVAL INTO THE ACTIVE FLIGHT PLAN Loading an arrival into the active ight plan using the PROC Key 1 Press the PROC Key The Procedures Window is displayed 2 Highlight S...

Page 252: ...name city and press the ENT Key 3 Press the FMS Knob then turn the large FMS Knob to highlight the Arrival The arrival is previewed on the map 4 Turn the small FMS Knob to view the available arrivals...

Page 253: ...ument approach procedures Only one approach can be loaded at a time in a ight plan If an approach is loaded when another approach is already in the active ight plan the new approach replaces the previ...

Page 254: ...using published LNAV VNAV minima LPV GPS approach using published LPV minima Table 5 9 Approach Types LOADING AN APPROACH INTO THE ACTIVE FLIGHT PLAN Loading an approach into the active ight plan usin...

Page 255: ...HT MANAGEMENT Figure 5 91 Approach Selection Destination Airport Approach Preview Available Procedure Actions Approach Choices Loaded Procedures Figure 5 92 Approach Loading Loaded Approach Selected A...

Page 256: ...plan from the Nearest Airport Page 1 Select the Nearest Airports Page 2 Press the FMS Knob then turn the large FMS Knob to highlight the desired nearest airport The airport is previewed on the map 3 S...

Page 257: ...of the approach REMOVING AN APPROACH FROM THE ACTIVE FLIGHT PLAN When plans change while ying IFR approaches can be easily removed from the Active Flight Plan Removing an approach from the active igh...

Page 258: ...is established to this x until an altitude of 6 368 feet reached After reaching 6 368 feet a direct to is established to the published x in this case MOGAL If the aircraft altitude is above the speci...

Page 259: ...r pilot Departure Time local Ground Speed Fuel Flow Fuel On Board Aircraft Calibrated Airspeed Indicated Altitude Barometric Pressure Total Air Temperature Softkeys Automatic Manual Page Mode Flight P...

Page 260: ...ight plan these default to the endpoints of the active leg Some of the calculated trip statistics are dashed when the selected leg of the active ight plan has already been own Desired Track DTK DTK i...

Page 261: ...ime to go Fuel required for trip FUEL REQ This value is calculated by multiplying the time to go by the fuel ow Total range at entered fuel ow TOTAL RANGE This value is calculated by multiplying the t...

Page 262: ...ftkey or press the MENU Key highlight Waypoints Mode and press the ENT Key The cursor is positioned in the waypoint eld directly below the FPL eld 2 Turn the FMS knobs to select the desired waypoint o...

Page 263: ...Fuel Calculation Empty Weight Softkey selects Basic Empty Weight Entering basic empty weight 1 Select the EMPTY WT Softkey or press the MENU Key highlight Set Basic Empty Weight and press the ENT Key...

Page 264: ...Press the FMS Knob to activate the cursor and highlight the FUEL ON BOARD eld 2 Turn the small FMS Knob to enter the fuel on board 3 Press the ENT Key to con rm the entry Synchronizing the fuel on boa...

Page 265: ...n the aircraft weight is displayed in amber If the estimated landing weight is greater than the maximum allowable landing weight then the estimated landing weight is displayed in amber If the estimate...

Page 266: ...times when RAIM is not available RAIM prediction must be initiated manually if there is concern over WAAS coverage at the destination or some other reason that compromises navigation precision If RAIM...

Page 267: ...Status Page 2 Press the FMS Knob The RAIM Prediction WAYPOINT eld is highlighted 3 Press the MENU Key highlight Set WPT to Present Position and press the ENT Key 4 Press the ENT Key to accept the way...

Page 268: ...Based Augmentation System SBAS provides increased navigation accuracy when available SBAS can be enabled or disabled manually on the GPS Status Page Figure 5 99 SBAS Display Active SBAS Softkey displa...

Page 269: ...the AUX GPS Status Page 2 Press the FMS Knob The SBAS SELECTION WAAS eld is highlighted 3 Press the ENT Key to disable SBAS Press the ENT Key again to enable SBAS Figure 5 100 SBAS Display Disabled S...

Page 270: ...KMKC to KCOS led using the TIFTO2 departure various Victor Airways and the DBRY1 arrival with the transition at TBE The ight plan includes an enroute altitude of 12 000 feet an LPV WAAS approach sele...

Page 271: ...119 FLIGHT MANAGEMENT 3 ATC now assigns routing to joinV4 A heading of 290 is assigned to interceptV4 The aircraft turns to heading 290 as seen in Figure 5 102 Figure 5 102 Assigned Heading of 290 4 E...

Page 272: ...ired ight plan insertion point SLN as shown in Figure 5 103 When the V4 entry point TOP is inserted it is placed immediately above the highlighted waypoint SLN Figure 5 103 Begin Adding V4 to the Flig...

Page 273: ...light Plan e With SLN still highlighted as in Figure 5 105 turn the small FMS Knob clockwise The Waypoint Information Page is displayed and the LD AIRWY Softkey is now available f Select the LD AIRWY...

Page 274: ...splayed as in Figure 5 107 Figure 5 107 List of Available Exits for V4 i If necessary turn either FMS Knob to select the desired exit In this case Salina VOR SLN is selected as in Figure 5 107 j Press...

Page 275: ...n the Flight Plan 5 Making V4 the active leg of the ight plan a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to highlight SLN The TO waypoint of the leg is selected in order to...

Page 276: ...leg Note the phase of ight remained inTerminal TERM mode up to this point because a departure leg was active Since a leg after the departure is now active the current CDI ight phase is ENR Enroute an...

Page 277: ...As the CDI approaches center the aircraft turns onto the active leg as seen in Figure 5 112 Figure 5 112 Turn on to Active Leg 8 At SLN Victor Airway 244 V244 is intercepted Turn prompts are displaye...

Page 278: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 00 Rev A 5 126 FLIGHT MANAGEMENT 9 As seen in Figure 5 114 V244 is now the active ight plan leg Figure 5 114 V244 Now Active Leg...

Page 279: ...11 ATC grants clearance to proceed direct to the OPSHN intersection to begin the arrival procedure ATC advises to expect an altitude of 10 000 feet at OPSHN a Press the FMS Knob to activate the curso...

Page 280: ...0 feet is entered as requested by ATC f Press the ENT Key The cursor is now displayed in the VNV offset eld as shown in Figure 5 118 Figure 5 118 Enter VNV Offset Distance g Enter the offset or distan...

Page 281: ...Note the Direct to waypoint is within the loaded arrival procedure therefore phase of ight scaling for theCDI changes to Terminal Mode and is annunciated by displaying TERM on the HSI NOTE If the loa...

Page 282: ...ould be highlighted as shown in Figure 5 120 Figure 5 120 Proceudures Window c Press the ENT Key A list of available approaches for the destination airport is displayed as in Figure 5 121 Figure 5 121...

Page 283: ...roach is displayed as in Figure 5 122 Figure 5 122 List of Available Transitions f Turn either FMS Knob to select the desired transition In this case the Initial Approach Fix IAF at HABUK is used g Pr...

Page 284: ...e used in computing vertical guidance a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to place the cursor in the altitude eld associated with the IAF at HABUK as in Figure 5 124...

Page 285: ...aypoints back to where the previous altitude value was entered for OPSHN Altitude constraint values associated with the Final Approach Fix FAF and waypoints beyond the FAF cannot be designated for ver...

Page 286: ...peed eld VS TGT as shown in Figure 5 127 b At this point the descent vertical speed can be selected or the FPA can be selected Turn the large FMS Knob to select the desired selection eld then turn the...

Page 287: ...al speed required to reached the selected altitude TheVertical Deviation Indicator VDI and the RequiredVertical Speed Indicator RVSI are now displayed on the PFD as shown in Figure 5 129 Figure 5 128...

Page 288: ...e 5 130 Figure 5 130 VDI RVSI Showing Correctly Established Descent Align Actual Vertical Speed with Required Vertical Speed Keep Vertical Deviation Pointer Centered 17 When the aircraft is one minute...

Page 289: ...ching OPSHN The upcoming turn and next heading are annunciated at the top left of the PFD as seen in Figure 5 132 Initiate the turn and maneuver the aircraft on a track through the turn radius to inte...

Page 290: ...re is now active Figure 5 133 Tracking the OPSHN to FSHER Leg 20 The ight continues through the arrival procedure to PYNON see Figure 5 134 At a point 31 nm from the destination airport the phase of i...

Page 291: ...190 00709 00 Rev A Garmin G1000 Pilot s Guide for the Socata TBM 850 5 139 FLIGHT MANAGEMENT Figure 5 134 Approaching PYNON...

Page 292: ...ogressed through the nal waypoint of the arrival and the ight plan has automatically sequenced to the IAF as the active leg activating the approach procedure see Figure 5 135 Figure 5 135 Approach is...

Page 293: ...TBM 850 5 141 FLIGHT MANAGEMENT 22 The IAF is the next waypoint At the TOD establish a descent vertical speed as previously discussed in Step 16 The aircraft altitude is 9 000 feet upon reaching HABUK...

Page 294: ...and is used much like a localizer when ying an ILS approach The RVSI is no longer displayed and the VDI changes to the Glidepath Indicator as shown in Figure 5 138 when the nal approach course become...

Page 295: ...e 6 368 feet after crossing the MAP a direct to is established to this x until an altitude of 6 368 feet reached After reaching 6 368 feet a direct to is established to the published x in this case MO...

Page 296: ...ng is suspended past the MAP Select the SUSP Softkey on the PFD to resume automatic waypoint sequencing through the missed approach procedure A direct to is initiated to MOGAL which is the Missed Appr...

Page 297: ...ntinues climbing to AT or ABOVE 10 000 feet at MOGAL A holding pattern is established at the MAHP MOGAL as shown in Figure 5 141 Figure 5 141 Establishing the Holding Pattern 27 The aircraft maintains...

Page 298: ...ading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS WAAS Mode due to the lack of satellite measurements needed to determine...

Page 299: ...GPS Navigation Lost Message Dead Reckoning Annunciation Subdued Aircraft Symbol Nav Data Bar All data except Active Leg TAS and DTK are in yellow Dead Reckoning Annunciaion Wind Data Wind Data Bearin...

Page 300: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 00 Rev A 5 148 FLIGHT MANAGEMENT BLANK PAGE...

Page 301: ...on the Multi Function Display MFD and the Primary Flight Display PFD Inset Map The GDL 69A can also receive XM Satellite Radio entertainment services Both weather data and entertainment programming op...

Page 302: ...d on the website Follow the instructions provided by XM Satellite Radio services 2 Select the next to last page in the AUX page group 3 Select the INFO Softkey to display the XM Information Page 4 Ver...

Page 303: ...ay Enabled When a weather product is active on the Weather Data Link Page or the Navigation Map Page the age of the data is displayed on the screen The age of the product is based on the time differen...

Page 304: ...data is refreshed at intervals that are de ned and controlled by XM Satellite Radio and its data vendors Weather Product Symbol Expiration Time Minutes Refresh Rate Minutes NEXRAD 30 5 Cloud Top CLD T...

Page 305: ...ap Page Weather Data Link Page Weather Information Page AUX Trip Planning Page Nearest Page Group Flight Plan Pages NEXRAD Cloud Top CLD TOP Echo Top ECHO TOP XM Lightning LTNG Cell Movement CELL MOV...

Page 306: ...ETAR LEGEND SFC OFF CYCLONE 24 HR 36 HR 12 HR BACK LEGEND CURRENT 48 HR OFF 9000 12000 6000 BACK LEGEND 3000 15000 SFC PREV OFF NEXT 27000 30000 24000 BACK LEGEND 21000 33000 18000 PREV OFF NEXT 42000...

Page 307: ...selections 5 Turn the small FMS Knob to scroll though options for each product ON OFF range settings etc 6 Press the ENT Key to select an option 7 Press the FMS Knob or CLR Key to return to the Weathe...

Page 308: ...ENT Key Figure 6 5 4 Turn the small FMS Knob to select the Weather Group and press the ENT Key Figure 6 6 5 Turn the large FMS Knob or press the ENT Key to scroll though product selections Figure 6 7...

Page 309: ...e legends if more are available than t in the window 4 To remove the Legend Window select the LEGEND Softkey the ENT or the CLR Key or press the FMS Knob Additional information about the following can...

Page 310: ...D network provides important information about severe weather for air traf c safety NEXRAD data is not real time The lapsed time between collection processing and dissemination of NEXRAD images can be...

Page 311: ...vidual radar sweeps The display of the information is color coded to indicate the weather severity level All weather product legends can be viewed on the Weather Data Link Page For the NEXRAD legend s...

Page 312: ...ve to re ectivity Z NEXRAD measures the radar re ectivity ratio or the energy re ected back to the radar receiver designated by the letter Z The value of Z increases as the returned signal strength in...

Page 313: ...en the radar antenna points directly at the sun Interference from buildings or mountains which may cause shadows Metallic dust from military aircraft which can cause alterations in radar scans NEXRAD...

Page 314: ...ly exclusive with Cloud Tops and NEXRAD Echo Tops data shows the location elevation and direction of the highest radar echo The highest radar echo does not indicate the top of a storm or clouds rather...

Page 315: ...ops use the same color scaling to represent altitude display of these weather products is mutually exclusive When Echo Tops is activated NEXRAD and Cloud Tops data are removed Figure 6 14 ECHO TOPS Le...

Page 316: ...6 15 Cloud Tops Data Displaying Cloud Tops information 1 Select the Weather Data Link Page with the FMS Knob 2 Select the CLD TOP Softkey To display the Cloud Tops legend select the LEGEND Softkey whe...

Page 317: ...ws the approximate location of cloud to ground lightning strikes A strike icon represents a strike that has occurred within a two kilometer region The exact location of the lightning strike is not dis...

Page 318: ...en XM Lightning is selected for display Figure 6 18 Lightning Legend CELL MOVEMENT Cell Movement data shows the location and movement of storm cells as identi ed by the ground based system Cells are r...

Page 319: ...vigation Map Setup Menu see Setting Up XM Satellite Weather To display the Cell Movement legend on the Weather Data Link Page select the LEGEND Softkey when Cell Movement is selected for display Figur...

Page 320: ...the SIG AIR Softkey 3 To view the text of the SIGMET or AIRMET press the RANGE Knob and move the Map Pointer over the icon 4 Press the ENT key The gure below shows a sample of SIGMET text To display t...

Page 321: ...s are shown as colored ags at airports that provide them Figure 6 23 METAR Flags on the Weather Data Link Page Instructions for Viewing METAR and TAF Text Selected Airport TAF Terminal Area Forecast i...

Page 322: ...nter the desired airport and press the ENT Key 5 Scroll through the METAR and TAF text with the FMS Knob or the ENT Key Scroll through all of the METAR text to get to the TAF text TAF Text METAR Symbo...

Page 323: ...ast information is available for current and forecast weather conditions Forecasts are available for intervals of 12 24 36 and 48 hours Figure 6 26 Surface Analysis Data 36 Hour Displaying Surface Ana...

Page 324: ...are selected for display Figure 6 27 Surface Analysis Legend FREEZING LEVEL Freezing Level data shows the color coded contour lines for the altitude and location at which the rst isotherm is found Whe...

Page 325: ...Figure 6 29 Freezing Level Legend WINDS ALOFT Winds Aloft data shows the forecast wind speed and direction at the surface and at selected altitudes Altitude can be displayed in 3000 foot increments up...

Page 326: ...ocata TBM 850 190 00709 00 Rev A 6 26 HAZARD AVOIDANCE Figure 6 30 Winds Aloft at 27 000 Feet To display the Winds Aloft legend select the LEGEND Softkey when Winds Aloft is selected for display Figur...

Page 327: ...tornadoes severe thunderstorms ood conditions and other natural disasters Figure 6 32 County Flood and Thunderstorm Warnings Thunderstorm Warnings Flood Warnings Displaying County Warning information...

Page 328: ...canes and their projected tracks Figure 6 34 Cyclone Data Selected for Display Cyclone Displaying cyclone hurricane track information 1 Select the Weather Data Link Page with the FMS Knob 2 Select the...

Page 329: ...ather behind a storm Weather Alert that looks ahead for intense cell activity in the 80 320 nm range even if these ranges are not being monitored PRINCIPLES OF PULSED AIRBORNE WEATHER RADAR The term R...

Page 330: ...The radar is only capable of seeing what is inside the boundaries of the beam The gure below depicts a radar beam s characteristics The gure illustrates vertical dimensions of the radar beam although...

Page 331: ...n of the radar energy is re ected back to the antenna However much of the energy is absorbed If precipitation is very heavy or covers a large area the signal may not reach completely through the area...

Page 332: ...are raindrops wet snow or wet hail The larger the raindrop the better the re ectivity The size of the precipitation droplet is the most important factor in radar re ectivity Because large drops in a...

Page 333: ...display However rough or choppy water is a better re ector and provides stronger returns from the downwind sides of the waves Mountains also provide strong return signals to the antenna but also bloc...

Page 334: ...Boundary 9 16 ft for 10 antenna Figure 6 40 MPEL Boundary BASIC ANTENNA TILT SETUP The following discussion is a simple method for setting up the weather radar antenna tilt for most situations It is n...

Page 335: ...range to 60 miles may be more helpful Closely monitor anything that enters the display Also after setting up the antenna tilt angle as described previously ground returns can be monitored for possibl...

Page 336: ...drafts in thunderstorms carry water through the cloud The more severe the drafts the greater the number and size of the precipitation droplets With this in mind the following interpretations can be ma...

Page 337: ...target return may also indicate turbulence appearing as hooks ngers or scalloped edges These irregularities may be present in green areas with no yellow red or magenta areas and should be treated as h...

Page 338: ...ften have not shown shapes different from those of a normal thunderstorm display HAIL Hail results from updrafts carrying water high enough to freeze Therefore the higher the top of a thunderstorm the...

Page 339: ...round no personnel or objects should be within 11 feet of the antenna CAUTION In Standby mode the antenna is parked at the center line It is always a good idea to put the radar in Standby mode before...

Page 340: ...r enters the Standby Mode a Select the WEATHER Softkey A con rmation window is displayed Figure 6 46 Con rming Activating Radar b Turn the small FMS Knob to highlight YES and press the ENT Key to cont...

Page 341: ...s the ENT Key 2 Press the ENT Key 3 Turn the small FMS Knob to place the Bearing Line on the desired storm cell or other area to be vertically scanned Figure 6 47 Bearing Line on Horizontal Scan Beari...

Page 342: ...eezing level of the storm The best way to nd this point is to use the Vertical Scan feature The antenna tilt angle can be centered on the strongest return area in the vertical scan to get a more accur...

Page 343: ...d and display the Tilt Line If theTilt Line is not displayed press the MENU Key and turn the large FMS Knob to select ShowTilt Line Press the ENT Key 2 Turn the small FMS Knob to adjust the antenna ti...

Page 344: ...sity of precipitation 1 Select the GAIN Softkey to activate the cursor in the GAIN eld 2 Turn the small FMS Knob to adjust the gain for the desirable level The gain setting is visible in the GAIN eld...

Page 345: ...he ENT Key Figure 6 51 Selecting Sector Scan Position 3 Turn the small FMS Knob to place the Bearing Line in the desired position The location of the Bearing Line becomes the center point of the Secto...

Page 346: ...tor Scan ANTENNA STABILIZATION 1 To activate or deactivate the antenna stabilization select the MODE Softkey 2 Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softk...

Page 347: ...tenuates the radar energy All these factors have an effect on the return intensity The more energy that dissipates the lesser the displayed intensity of the return Accuracy of the displayed intensity...

Page 348: ...imate azimuth of the detected returns If a Weather Alert is detected within 10 of the aircraft heading an alert is displayed on the PFD in the Messages Window If the antenna tilt is adjusted too low a...

Page 349: ...rgets can be recognized more easily As previously discussed the type and orientation of the target in relation to the aircraft affects the intensity displayed When the weather radar system is in eithe...

Page 350: ...he INSET Softkey for the PFD Inset Map then select the STRMSCP Softkey These pages can also display cell or strike data using the yellow lightning strike symbology shown in Table 6 5 Lightning Age Sym...

Page 351: ...display of Stormscope data on or off STRMSCP MODE Selects the CELL or STRIKE mode of lightning activity Cell mode identi es clusters or cells of electrical activity Strike mode indicates the approxim...

Page 352: ...elect the Weather group 4 Press the ENT Key The cursor ashes on STRMSCP LTNG 5 Turn the large FMS Knob to select STRMSCP MODE 6 Turn the small FMS Knob to change between CELL and STRIKE options When a...

Page 353: ...ion of Stormscope lightning data can be behind the aircraft and therefore not visible on the Navigation Map Since the range for Stormscope data is 400 nm diameter total 200 nm in front and 200 nm behi...

Page 354: ...e FMS Knob to return to the Navigation Map Page To change the display range on the Navigation Map Page turn the RANGE Knob clockwise to zoom out or counter clockwise to zoom in SELECTING THE STORMSCOP...

Page 355: ...Stormscope Page Or 1 Select the Stormscope Page 2 Press the MENU Key 3 Turn the small FMS Knob to choose between CELL and STRIKE options 4 When an item is selected press the ENT Key If heading input i...

Page 356: ...ftkey The 360 and ARC softkeys are displayed 3 Select the 360 Softkey to display a 360 viewing area or select the ARC Softkey to display a 120 viewing area 4 Select the BACK Softkey to return to the S...

Page 357: ...aircraft position and altitude with reference to a database that may contain inaccuracies Terrain and obstructions are shown only if they are in the database Terrain and obstacle information should be...

Page 358: ...or within 100 ft below the aircraft altitude Yellow obstacle is between 100 ft and 1000 ft below the aircraft altitude Table 6 6 Terrain Proximity Terrain Obstacle Colors and Symbology Terrain and obs...

Page 359: ...ly Customizing terrain and obstacle display on the Navigation Map Page 1 Select the Navigation Map Page 2 Press the MENU Key 3 With Map Setup highlighted press the ENT Key Figure 6 64 4 Turn the small...

Page 360: ...raft Altitude TERRAIN PROXIMITY PAGE The Terrain Proximity Page is specialized to show terrain and obstacle data in relation to the aircraft s current altitude without clutter from the basemap Aviatio...

Page 361: ...Terrain Between 100 and 1000 Below the Aircraft Altitude Red Terrain Above or Within 100 Below the Aircraft Altitude Black Terrain More than 1000 Below the Aircraft Altitude Terrain Legend Map Range R...

Page 362: ...information provided from the GPS receiver to provide a horizontal position and altitude GPS altitude is derived from satellite measurements GPS altitude is converted to a mean sea level MSL based al...

Page 363: ...tial Impact Points Obstacle Location 1000 AGL 1000 AGL 1000 AGL 1000 AGL WARNING Red obstacle is above or within 100 below current aircraft altitude CAUTION Yellow obstacle is between 100 and 1000 bel...

Page 364: ...ange setting made for the Navigation Map If the maximum range for obstacle display on the Navigation Map is adjusted to below 20 nm the highest obstacle display range settings on the other applicable...

Page 365: ...tomatically zooms in to the closest potential point of impact on the TAWS Page Aircraft orientation on this map is always heading up unless there is no valid heading Two views are available relative t...

Page 366: ...errain Between 100 and 1000 Below the Aircraft Altitude Red Terrain Above or Within 100 Below the Aircraft Altitude Black Terrain More than 1000 Below the Aircraft Altitude Terrain Legend Map Range Ri...

Page 367: ...ed Table 6 8 shows TAWS alert types with corresponding annunciations and aural messages When an alert is issued annunciations appear on the PFD and MFD The TAWS Alert Annunciation is shown to the uppe...

Page 368: ...FD and MFD Figure 6 79 TAWS Alerting Disabled TAWS Inhibited Annunciation Inhibiting enabling TAWS alerting 1 Select the TAWS Page 2 Press the MENU Key 3 Select Inhibit TAWS or Enable TAWS depending o...

Page 369: ...r Obstacle Obstacle Pull Up Pull Up Reduced Required Terrain Clearance Caution RTC or Terrain Ahead Terrain Ahead or Caution Terrain Caution Terrain Imminent Terrain Impact Caution ITI or Terrain Ahea...

Page 370: ...noti cation when the aircraft is determined to be closing descending upon terrain at an excessive speed The following gure shows the parameters for the alert as de ned by TSO C151b 6000 5500 5000 450...

Page 371: ...PACT Imminent Terrain 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 aircraft s projected path ITI and IOI...

Page 372: ...eshold During the nal descent algorithms set a threshold for alerting based on speed distance and other parameters 700 600 500 400 300 200 100 Height Above Terrain Feet Distance From Destination Airpo...

Page 373: ...lay NCR alerting is only active when departing from an airport and when the following conditions are met Height above the terrain is less than 700 feet Distance from the departure airport is 2 nm or l...

Page 374: ...tem Testing is disabled when ground speed exceeds 30 knots Alert Type PFD MFD Alert Annunciation TAWS Page Annunciation Aural Message System Test in Progress TAWS TEST None System Test Pass None None...

Page 375: ...inimums Should the navigation solution become degraded or if the aircraft is out of the database coverage area the annunciation TAWS N A is generated in the annunciation window and on the TAWS Page Th...

Page 376: ...isplayed according to TCAS symbology using four different symbols TAS Symbol Description Non Threat Traf c Proximity Advisory PA Traf c Advisory TA Traf c Advisory Off Scale Table 6 12 TAS Symbol Desc...

Page 377: ...Page select the STANDBY Softkey Or 1 Press the MENU Key and turn the small FMS knob to select Standby Mode 2 Press the ENT Key to place the KTA 870 in the Standby mode System Self Test 1 Set the range...

Page 378: ...no valid heading Map range is adjustable with the RANGE Knob from 2 to 40 nm as indicated by the map range rings The traf c mode and altitude display mode are annunciated in the upper left corner DISP...

Page 379: ...ies Non Threat Traf c The Navigation Map Page Setup Menu also controls the display of traf c The setup menu controls the map range settings Traf c data symbols and labels can be decluttered from the d...

Page 380: ...af c display on the Navigation Map Page 1 Select the Navigation Map Page 2 Press the MENU Key 3 With Map Setup highlighted press the ENT Key Figure 6 87 4 Turn the small FMS Knob to select the Traf c...

Page 381: ...6 81 HAZARD AVOIDANCE 7 Press the ENT Key to select an option 8 Press the FMS Knob or CLR Key to return to the Navigation Map Page Figure 6 88 Navigation Map Page Setup Menu Figure 6 87 Navigation Ma...

Page 382: ...ining displayed until no TAs are detected in the area The PFD Inset Map is automatically displayed with TA traf c Figure 6 90 Traf c Annunciation PFD Inset Map Displays When TA is Detected SYSTEM STAT...

Page 383: ...mation appear in a banner at the lower left corner of maps on which traf c can be displayed Traf c Status Banner Annunciation Description TA OFF SCALE A Traf c Advisory is outside the selected display...

Page 384: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 00 Rev A 6 84 HAZARD AVOIDANCE BLANK PAGE...

Page 385: ...0 has two ight directors each operating within an IAU and referred to as pilot side and copilot side Commands for the selected ight director are displayed on both PFDs The ight directors provide Comma...

Page 386: ...ode in 1 increments on the Horizontal Situation Indicator HSI of the corresponding PFD Press to re center the Course Deviation Indicator CDI and return course pointer directly TO the bearing of the ac...

Page 387: ...r Takeoff on ground or Go Around in air Mode If an approach procedure is loaded this switch also activates the missed approach when the selected navigation source is GPS or when the navigation source...

Page 388: ...when the autopilot is engaged Control Pressed Modes Selected Lateral Vertical FD Key Roll Hold default ROL Pitch Hold default PIT AP Key Roll Hold default ROL Pitch Hold default PIT CWS Button Roll H...

Page 389: ...per statuses are shown in the center of the AFCS Status Box Lateral ight director modes are displayed on the left and vertical on the right Armed modes are displayed in white and active in green GPS i...

Page 390: ...iation and annunciator light indicate loss of sensor ADC or navigation data VOR LOC GPS VNV WAAS required to compute commands When such a loss occurs the system automatically begins to roll the wings...

Page 391: ...Both PFDs show the same Command Bar format Figure 7 5 Single cue Command Bars Aircraft Symbol Command Bars Aircraft Symbol Command Bars Figure 7 6 Cross pointer Command Bars Changing Command Bar forma...

Page 392: ...raft vertical speed may be used to climb descend to the Selected Altitude VS Key VS nnnn FPM 4000 to 3000 fpm 100 fpm Flight Level Change IAS Hold Maintains the current aircraft airspeed in IAS or Mac...

Page 393: ...Pitch Hold Mode the ight director maintains a constant pitch attitude the pitch reference The pitch reference is set to the aircraft pitch attitude at the moment of mode selection If the aircraft pit...

Page 394: ...n ashing for up to 10 seconds and the appearance of the white ALT annunciation The Selected Altitude is shown as the Altitude Reference beside the ALTS annunciation At 50 feet from the Selected Altitu...

Page 395: ...e Capture Mode see Figure 7 8 Selected Altitude Capture Mode automatically transitions to Altitude Hold Mode when the altitude error is less than 50 feet In this case the Selected Altitude becomes the...

Page 396: ...o displayed above the Vertical Speed Indicator A Vertical Speed Reference Bug corresponding to the Vertical Speed Reference is shown on the indicator CHANGING THE VERTICAL SPEED REFERENCE The Vertical...

Page 397: ...Flight Level Change Mode is indicated by a green FLC annunciation beside the Airspeed Reference in the AFCS Status Box The Airspeed Reference is also displayed directly above the Airspeed Indicator a...

Page 398: ...is not changed To adjust the Altitude Reference in this case the CWS Button must be pressed again after the Selected Altitude is reached Airspeed Reference units can be manually toggled between IAS a...

Page 399: ...and Bars provide vertical pro le guidance based on speci ed altitudes entered manually or loaded from the database at waypoints in the active ight plan or vertical direct to The appropriate VNV ight c...

Page 400: ...start to ash Flashing continues until acknowledged or the descent path is intercepted If the descent is not con rmed by the time of interception Vertical Path Tracking Mode remains armed and the desce...

Page 401: ...cking Mode VNV Target Altitude Capture Armed Vertical Path Tracking Active If the altimeter barometric setting is adjusted while Vertical Path Tracking is active the ight director increases decreases...

Page 402: ...an active vertical direct to Unless VNV is disabled Vertical Path Tracking Mode and the appropriate altitude capture mode become armed following the reversion to Pitch Hold Mode to allow for possible...

Page 403: ...white ALT annunciation The VNV Target Altitude is shown as the Altitude Reference beside the ALTV annunciation and remains displayed above the Vertical Speed Indicator The Required Vertical Speed Ind...

Page 404: ...ect to a waypoint not in the ight plan 2 Ensure that GPS is the selected navigation source use the CDI Softkey to cycle through navigation sources if necessary 3 Press the APR Key Upon reaching the gl...

Page 405: ...on source use the CDI Softkey to cycle through navigation sources if necessary 3 Press the APR Key Or 1 Ensure that GPS is the selected navigation source use the CDI Softkey to cycle through navigatio...

Page 406: ...off This mode can be selected only while on the ground by pushing the GA Switch The ight director Command Bars assume a wings level pitch up attitude Pressing the GA Switch while in the air activates...

Page 407: ...n LOC Capture Track No Glideslope LOC 25 Capture 10 Track Backcourse Capture Track Captures and tracks a localizer signal for backcourse approaches BC Key BC 25 Capture 10 Track Approach GPS Captures...

Page 408: ...able 7 4 Roll Hold Mode Responses Figure 7 24 Roll Hold Mode Annunciation CHANGING THE ROLL REFERENCE The roll reference can be changed by pressing the CWS Button establishing the desired bank angle t...

Page 409: ...rrent heading The Selected Heading is adjusted using the HDG Knob Pressing the CWS Button and hand ying the aircraft does not change the Selected Heading The autopilot guides the aircraft back to the...

Page 410: ...NAV Key is pressed the selected mode is armed If the CDI is less than one dot Navigation Mode is automatically captured when the NAV Key is pressed The armed annunciation appears in white to the left...

Page 411: ...elected ight director CRS1 for the pilot side CRS2 for the copilot side Pressing the CWS Button and hand ying the aircraft does not change the Selected Course while in Navigation Mode The autopilot gu...

Page 412: ...ft of the active lateral mode If the CDI is less than one dot the LOC is automatically captured when the APR Key is pressed VOR Approach Mode VAPP provides greater sensitivity for signal tracking than...

Page 413: ...ded into the active ight plan 3 Ensure the corresponding LOC frequency is tuned 4 Press the APR Key If the following occurs the ight director reverts to Roll Hold Mode wings rolled level Approach Mode...

Page 414: ...the BC Key is pressed The ight director creates roll steering commands from the Selected Course and deviation when in Backcourse Mode LOC2 is Selected Navigation Source Pitch Hold Mode Active Backcou...

Page 415: ...is uses pitch rate to stabilize the aircraft pitch attitude during ight director maneuvers Flight director pitch commands are rate and attitude limited combined with pitch damper control and sent to t...

Page 416: ...ly of the autopilot and the yaw damper annunciator light is illuminated Autopilot and yaw damper status are displayed in the center of the AFCS Status Box Engagement is indicated by green AP and YD an...

Page 417: ...onds upon disengagement Figure 7 34 Yaw Damper Disengagement Automatic autopilot disengagement is indicated by a ashing red and white AP annunciation and by the autopilot disconnect aural alert which...

Page 418: ...des used during a ight In this scenario the aircraft departs Charles B Wheeler Downtown Airport KMKC enroute to Colorado Springs Airport KCOS After departure the aircraft climbs to 12 000 ft and airwa...

Page 419: ...vate Vertical Speed Mode The Vertical Speed Reference may be adjusted after Vertical Speed Mode is selected using the NOSE UP DN Wheel or pushing the CWS Button while hand ying the aircraft to establi...

Page 420: ...000 Pilot s Guide for the Socata TBM 850 190 00709 00 Rev A 7 36 AUTOMATIC FLIGHT CONTROL SYSTEM Figure 7 37 Departure Selected Altitude of 12 000 MSL 1 2 3 4 HDG Mode VS Mode ALT Mode TO Mode T O M o...

Page 421: ...he navigation source to VOR c Use the CRS1 or CRS2 Knob to set the Selected Course to the desired value 255 Note that at this point the ight director is still in Heading Select Mode and the autopilot...

Page 422: ...ransition from VOR to GPS Navigation Mode a Press the CDI Softkey until GPS is the selected navigation source b Press the NAV Key to activate GPS Navigation Mode The autopilot guides the aircraft alon...

Page 423: ...t Level Change Mode is used in the example Flight Level Change descent 1 Select Flight Level Change Mode a Using the ALT SEL Knob set the Selected Altitude to 10 000 feet b Press the FLC Key to activa...

Page 424: ...annunciation begins ashing do one of the following Press the VNV Key Turn the ALT SEL Knob to adjust the Selected Altitude If the descent is not con rmed by the time of interception Vertical Path Tra...

Page 425: ...t maintains the Airspeed Reference 3 As the aircraft nears the Selected Altitude the ight director transitions to Selected Altitude Capture Mode indicated by the green ALTS annunciation ashing for up...

Page 426: ...CONTROL SYSTEM Figure 7 42 Non path Descent OPSHN 3 nm HABUK VNAV Target Altitude of 10 000 MSL VNAV Target Altitude of 9 000 MSL ALT Mode Planned Descent Path Selected Altitude of 9 400 MSL ALT Mode...

Page 427: ...odes a Ensure the appropriate localizer frequency is tuned b Press the APR Key when cleared for approach to arm Approach and Glideslope modes LOC and GS appear in white as armed mode annunciations c T...

Page 428: ...the approach into the ight plan 2 Press the APR Key once clearance for approach has been received GPS Approach Mode is activated and Glidepath Mode is armed 3 Once the glidepath is captured Glidepath...

Page 429: ...P annunciation ashing yellow for 5 seconds and the autopilot disconnect aural alert Flashes 5 sec 2 Start the climb to the prescribed altitude in the published Missed Approach Procedure in this case 1...

Page 430: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 00 Rev A 7 46 AUTOMATIC FLIGHT CONTROL SYSTEM Figure 7 45 Go Around Missed Approach 3 4 1 2 KCOS MOGAL GA Mode GPS NAV Mode...

Page 431: ...icated direction Elevator Mistrim Up Pitch Trim Failure or stuck MEPT Switch If AP engaged take control of the aircraft and disengage AP If AP disengaged move MEPT switches separately to unstick Yaw T...

Page 432: ...l overspeed protection becomes active Overspeed protection is provided in situations where the ight director cannot acquire and maintain the mode reference for the selected vertical mode without excee...

Page 433: ...choices and longer range coverage than commercial broadcast stations The Scheduler feature can be used to enter and display short term or long term reminder messages such as Switch fuel tanks Change...

Page 434: ...n KSFO airport Airport Hot Spots are outlined in magenta When panning over the airport features such as runway holding lines and taxiways are shown at the cursor Figure 8 1 SafeTaxi Depiction on the N...

Page 435: ...Map Setup Option 3 Turn the FMS Knob to select the Aviation Group and press the ENT Key 4 Turn the large FMS Knob to scroll through the Aviation Group options to SAFETAXI 5 Turn the small FMS Knob to...

Page 436: ...ates whether the databases are current out of date or not available The Power up Page shows the SafeTaxi database is current when the SafeTaxi Expires date is shown in white When the SafeTaxi cycle ha...

Page 437: ...gure 8 6 Expired SafeTaxi data is never disabled Select the DBASE Softkey for scrolling through the database information Scroll through the database with the FMS knob or ENT Key The SafeTaxi database...

Page 438: ...is before the effective date the EFFECTIVE date appears in yellow and the EXPIRES date appears in blue The EXPIRES date is the revision date for the next database cycle NOT AVAILABLE indicates that S...

Page 439: ...e selecting the SHW CHRT Softkey displays the available terminal chart and advances to the chart selection level of softkeys CHRT OPT CHRT INFO DP STAR APR WX NOTAM and GO BACK The chart selection sof...

Page 440: ...through the OPTIONS Menu to Show Chart 3 Press the ENT Key to display the chart Navigation Map Page OPTIONS Menu Waypoint Airport Information Page OPTIONS Menu Figure 8 8 Option Menus When no termina...

Page 441: ...e WPT Pages or Flight Plan Pages If a chart is available for the destination airport or the airport selected in the active ight plan the chart appears on the screen When no ight plan is active or when...

Page 442: ...ion choices 8 Turn either FMS Knob to scroll through the available charts 9 Press the ENT Key to complete the chart selection Figure 8 11 Approach Information Page Chart Selection Select Desired Appro...

Page 443: ...rtView diagram and the associated map in the WPT page group In the example shown the CHRT Softkey switches between the Gainesville FL KGNV Airport Diagram and the navigation map on the WPT Airport Inf...

Page 444: ...Taxiway Bravo on the Charlotte NC KCLT airport Another source for additional airport information is from the INFO Box above the chart for certain airports This information source is not related to th...

Page 445: ...ass B Chart is selected Pressing the ENT Key displays the Charlotte Class B Airspace Chart Figure 8 14 Figure 8 14 Airport Information Page Class B Chart Selected from INFO View Selecting the DP Softk...

Page 446: ...displays the Standard Terminal Arrival Chart if available Figure 8 16 Arrival Information Page Aircraft Not Shown Icon Change Range and Scroll Through the Chart With the Joystick Chart Not To Scale S...

Page 447: ...port weather frequency information and includes weather data such as METAR and TAF from the XM Data Link Receiver when available Weather information is available only when an XM Data Link Receiver is...

Page 448: ...luded in the ChartView database Selecting the NOTAM Softkey shows the local NOTAM information for selected airports when available When NOTAMS are not available the NOTAM Softkey label appears subdued...

Page 449: ...EATURES Figure 8 20 Airport Information Page Local NOTAMs Local NOTAM on This Airport NOTAM Softkey Selected Selecting the NOTAM Softkey again removes the NOTAMS information Selecting the GO BACK Soft...

Page 450: ...ADDITIONAL FEATURES CHART OPTIONS Selecting the CHRT OPT Softkey displays the next level of softkeys the chart options level Figure 8 7 Selecting the ALL Softkey shows the entire approach chart on the...

Page 451: ...EADER Softkey shows the header view approach chart brie ng strip on the screen Approach Chart Brie ng Strip Figure 8 22 Approach Information Page Header View Selecting the PLAN Softkey shows the appro...

Page 452: ...cent pro le strip Approach Chart Descent Pro le Strip Figure 8 24 Approach Information Page Pro le View Full Screen Width Selecting the MINIMUMS Softkey displays the minimum descent altitude visibilit...

Page 453: ...AL FEATURES If the chart scale has been adjusted to view a small area of the chart selecting the FIT WIDTH Softkey changes the chart size to t the available screen width Select FIT WDTH Softkey to Sho...

Page 454: ...large FMS Knob to highlight the AIRPORT INFO RUNWAYS or FREQUENCIES Box INFO Box shown 4 Turn the small FMS Knob to select the INFO Box choices If multiple choices are available scroll to the desired...

Page 455: ...ile viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS 2 Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 Turn the large FMS Knob to m...

Page 456: ...press the ENT Key Figure 8 29 Waypoint Information Page OPTIONS Menu 3 Turn the large FMS Knob to move to the COLOR SCHEME Option Figure 8 30 4 Turn the small FMS Knob to choose between Day Auto and N...

Page 457: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 00 Rev A 8 25 ADDITIONAL FEATURES Figure 8 30 Arrival Information Page Day View Figure 8 31 Arrival Information Page Night View...

Page 458: ...rmin authorized service center for con guration System is con gured for ChartView but no chart database is installed Contact Jeppesen for a ChartView database Normal operation ChartView database is va...

Page 459: ...chart data cycle has expired within the past week and the next chart cycle is available Chart data is out of date in yellow indicates charts are still viewable but approaching the disable date Chart...

Page 460: ...and is disabled until a revised issue of ChartView is installed Select the DBASE Softkey for scrolling through the database information Scroll through the database with the FMS knob or ENT Key The Cha...

Page 461: ...s the date that this database cycle is no longer viewable REGION and CYCLE NOT AVAILABLE in blue indicate that no ChartView data is available on the database card or no database card is inserted Figur...

Page 462: ...chart selection level of softkeys CHRT OPT CHRT INFO DP STAR APR WX and GO BACK The chart selection softkeys appear on the Airport Information Page Selecting the GO BACK Softkey reverts to the top le...

Page 463: ...rge FMS Knob to scroll through the OPTIONS Menu to Show Chart 3 Press the ENT Key to display the chart Navigation Map Page OPTIONS Menu Waypoint Airport Information Page OPTIONS Menu Figure 8 36 Optio...

Page 464: ...he WPT Pages or Flight Plan Pages If a chart is available for the destination airport or the airport selected in the active ight plan the chart appears on the screen When no ight plan is active or whe...

Page 465: ...the large FMS Knob to select the Approach Box 7 Turn the small FMS Knob to show the approach chart selection choices 8 Turn either FMS Knob to scroll through the available charts 9 Press the ENT Key...

Page 466: ...FliteCharts diagram and the associated map in the WPT page group In the example shown the CHRT Softkey switches between the Gainesville FL KGNV Airport Diagram and the navigation map on the WPT Airpor...

Page 467: ...airport information is from the INFO Box above the chart Figure 8 39 or to the right of the chart Figure 8 41 for certain airports This information source is not related to the INFO Softkey When the I...

Page 468: ...n Figure 8 41 ALTERNATE MINIMUMS is selected Pressing the ENT Key displays the IFR Alternate Minimums Chart Figure 8 42 Figure 8 42 Airport Information Page ALTERNATE MINIMUMS Selected from INFO View...

Page 469: ...8 37 ADDITIONAL FEATURES Selecting the STAR Softkey displays the Standard Terminal Arrival Chart if available Figure 8 44 Arrival Information Page Selecting the APR Softkey displays the approach char...

Page 470: ...ey to display the information windows AIRPORT INFO 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the INFO Box 4 Turn the small FMS Knob to select the INFO Box choi...

Page 471: ...ADDITIONAL FEATURES CHART OPTIONS Selecting the CHRT OPT Softkey displays the next level of softkeys the chart options level Figure 8 35 Selecting the ALL Softkey shows the entire chart on the screen...

Page 472: ...TURES Selecting the FIT WIDTH Softkey ts the width of the chart in the display viewing area In the example shown the chart at close range is replaced with the full width chart Figure 8 48 Approach Inf...

Page 473: ...ey alternates between removing and replacing the data window to the right Figure 8 49 Airport Information Page Full Screen and Info Window Select FULL SCN Softkey to Switch Between Chart on Full Scree...

Page 474: ...ile viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS 2 Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 Turn the large FMS Knob to m...

Page 475: ...press the ENT Key Figure 8 51 Waypoint Information Page OPTIONS Menu 3 Turn the large FMS Knob to move to the COLOR SCHEME Option Figure 8 52 4 Turn the small FMS Knob to choose between Day Auto and...

Page 476: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 00 Rev A 8 44 ADDITIONAL FEATURES Figure 8 52 Approach Information Page Day View Figure 8 53 Approach Information Page Night View...

Page 477: ...able current out of date or disabled See the table below for the various FliteCharts Power up Page displays and the de nition of each Power up Page Display De nition Blank Line G1000 system is not con...

Page 478: ...proaching the disable date When the 180 day grace period has expired Chart data is disabled in yellow indicates that the FliteCharts database has expired and is no longer viewable Chart Data N A appea...

Page 479: ...subdued and is unavailable until a revised issue of FliteCharts is installed Select the DBASE Softkey for scrolling through the database information Scroll through the database with the FMS knob or E...

Page 480: ...that this database cycle is no longer viewable REGION and CYCLE NOT AVAILABLE in blue indicate that FliteCharts database is not available on the database card or no database card is inserted Figure 8...

Page 481: ...r more information on speci c service packages visit www xmradio com ACTIVATING XM SATELLITE RADIO SERVICES The service is activated by providing XM Satellite Radio with either one or two coded IDs de...

Page 482: ...on the website Follow the instructions provided by XM Satellite Radio services 2 Select the Auxiliary Page Group 3 Select the next to last page in the AUX Page Group 4 Select the INFO Softkey to displ...

Page 483: ...nment features of the XM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select the displayed AUX XM Information P...

Page 484: ...list 1 While on the XM Radio Page select the CHNL Softkey 2 Select the CH Softkey to go up through the list in the Channel Box or move down the list with the CH Softkey Or 1 Press the FMS Knob to hig...

Page 485: ...els for a type of music or other contents One of the optional categories is PRESETS to view channels that have been programmed Selecting a category 1 Select the CATGRY Softkey on the XM Radio Page 2 S...

Page 486: ...ber to the active channel 4 Select the SET Softkey on the desired channel number to save the channel as a preset Figure 8 60 Accessing and Selecting XM Preset Channels Select PRESETS to Access the Pre...

Page 487: ...62 Scheduler Utility Page Entering a scheduler message 1 Select the AUX Utility Page 2 Press the FMS Knob momentarily to activate the ashing cursor 3 Turn the large FMS Knob to highlight the rst empty...

Page 488: ...momentarily to activate the ashing cursor 3 Turn the large FMS Knob to highlight the name eld of the scheduler message to be deleted 4 Press the CLR Key to clear the message text If the CLR Key is pr...

Page 489: ...lists cannot be edited from within the system Refer to the Garmin Aviation Checklist Editor ACE User s Guide for information on creating and editing checklists The optional Checklist functions are dis...

Page 490: ...select the desired checklist and press the ENT Key 6 Turn the FMS Knob to scroll through the checklist and highlight the desired checklist item has a hollow white box for checkmark The following color...

Page 491: ...checklist is highlighted Press the ENT Key to advance to the next checklist displayed 9 Select the EXIT Softkey or hold down the CLR Key momentarily to exit the Checklist Page and return to the page...

Page 492: ...activated Perform a quick check of the circuit breakers to ensure that power is applied to the Data Link Receiver For troubleshooting purposes check the LRU Information Box on the AUX System Status Pa...

Page 493: ...NO SIGNAL XM Radio Page active channel eld Weather Datalink Page center of page Loss of signal signal strength too low for receiver LOADING XM Radio Page active channel eld Acquiring channel audio or...

Page 494: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 00 Rev A 8 62 ADDITIONAL FEATURES BLANK PAGE...

Page 495: ...T Battery temperature over 70 C BLEED TEMP Bleed temperature high X X CABIN ALTITUDE Cabin altitude over 10 000 ft X CABIN DIFF PRESS Cabin pressure differential over 6 2 psi X DOOR Pilot or cabin doo...

Page 496: ...r running INERT SEP FAIL Inertial separator failure X X INERT SEP ON Inertial separator extended LOW LVL FAIL L R Low fuel level sensor failure for speci ed tank LOW VOLTAGE Battery voltage below 26 V...

Page 497: ...rator Window Text Condition ALT MISCOMP Difference in altitude sensors is 200 ft IAS MISCOMP If both airspeed sensors detect 35 knots this is inhibited If either airspeed sensor detects 35 knots and t...

Page 498: ...ADC The PFDs are displaying data from the cross side Air Data Computer XSIDE AHRS The PFDs are displaying data from the cross side Attitude Heading Reference System G1000 SYSTEM ANNUNCIATIONS When a...

Page 499: ...unciation Red X Figure A 4 G1000 System Failure Annunciations GDC 74B Air Data Computer GTX 33 D Transponder Or GIA 63W Integrated Avionics Units GDC 74B Air Data Computer GEA 71 Engine Airframe Unit...

Page 500: ...tion indicates an AHRS monitor has detected an abnormal ight parameter possibly caused by strong turbulence In this case the situation should correct itself within a few seconds If there is an actual...

Page 501: ...e aircraft systems ight conditions and other existing operational priorities must be considered when responding to a message Always use sound pilot judgment The Pilot s Operating Handbook POH takes pr...

Page 502: ...g Reducing power usage PFD1 KEYSTK PFD1 key name Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced...

Page 503: ...eci ed LRU PFD1 DB ERR PFD1 terrain database missing PFD2 DB ERR PFD2 terrain database missing MFD1 DB ERR MFD1 obstacle database error exists The MFD and or PFD detected a failure in the obstacle dat...

Page 504: ...FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced DB MISMATCH Aviation database version mis...

Page 505: ...e available and the audio panel may still be usable The G1000 system should be serviced when possible GMA2 SERVICE GMA2 needs service Return unit for repair GIA 63W MESSAGE ADVISORIES Message Comments...

Page 506: ...e COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced...

Page 507: ...nsfer key is stuck G S1 FAIL G S1 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced G S2 FAIL G S2 is inoperative G S1 SERVICE G...

Page 508: ...nformation to augment the lack of airspeed The G1000 system should be serviced AHRS2 TAS AHRS2 not receiving airspeed The 2 AHRS is not receiving true airspeed from the air data computer The AHRS reli...

Page 509: ...the 1 GMU 44 Heading is agged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced HDG FAULT AHRS2 magnetometer fault has occurred A fault has occurred in the 2 G...

Page 510: ...system should be serviced MANIFEST GDC2 software mismatch communication halted GCU 475 MESSAGE ADVISORIES Message Comments GCU CNFG GCU Con g error Con g service req d GCU 475 con guration settings do...

Page 511: ...s and reload airways as needed FPL TRUNC Flight plan has been truncated This occurs when a newly installed aviation database eliminates an obsolete approach or arrival used by a stored ight plan The o...

Page 512: ...Unavailable Parallel course selected A parallel course has been selected causing the vertical deviation to go invalid NO WGS84 WPT Non WGS 84 waypoint for navigation xxxx The selected waypoint xxxx do...

Page 513: ...itch If AP engaged take control of the aircraft and disengage AP If AP disengaged move the MEYT switch to unstick Yaw Damper Failure YD control failure AP still operative Roll Failure Roll axis contro...

Page 514: ...p Pull Up or ObstacleAhead Pull Up ObstacleAhead Pull Up Imminent Obstacle ImpactWarning IOI or ObstacleAhead Pull Up ObstacleAhead Pull Up or Obstacle Obstacle Pull Up Pull Up Reduced RequiredTerrain...

Page 515: ...GPS position or excessively degraded GPS signal None TAWS Not Available TAWS Availble is heard when suf cient GPS signal is re established System Test in progress None None System Test pass None None...

Page 516: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 00 Rev A A 22 APPENDIX A BLANK PAGE...

Page 517: ...D The aviation database may be installed from the Jeppesen supplied SD data card or copied to one of the Garmin supplied Supplemental Data Cards Contact Jeppesen www jeppesen com for subscription and...

Page 518: ...ducts will be downloaded to three Supplemental Data Cards with the exception of FliteCharts which is loaded on only one card Insert each Supplemental Data Card into the correct location shown in Figur...

Page 519: ...abases section of the Garmin website www garmin com Once the updated les have been downloaded from the website a PC equipped with an appropriate SD card reader is used to unpack and program the new da...

Page 520: ...essing the ENT Key or the right most softkey 4 Turn the large FMS Knob to select the AUX Page group on the MFD 5 Turn the small FMS Knob to select the System Status Page 6 Select the DBASE Softkey to...

Page 521: ...arometric setting BATT battery BC backcourse Bearing The compass direction from the present position to a destination waypoint BFO beat frequency oscillator BKSP backspace BRG bearing C center runway...

Page 522: ...Endurance Flight endurance or total possible ight time based on available fuel on board ENG engine ENGD engaged ENR enroute Enroute Safe Altitude The recommended minimum altitude within ten miles lef...

Page 523: ...GRS Garmin Reference System GS Ground speed GTX Garmin Transponder HA Hold Terminating at Altitude HDG heading Heading The direction an aircraft is pointed based upon indications from a magnetic compa...

Page 524: ...ch Point MASQ Master Avionics Squelch MAX maximum MAXSPD maximum speed overspeed MDA barometric minimum descent altitude MET manual electric trim METAR Meteorological Aviation Routine MEPT manual elec...

Page 525: ...Signi cant Meteorological Information Sim simulator SLP SKD slip skid SMBL symbol SPD speed SPI Special Position Identi cation SPKR speaker SQ squelch SRVC SVC service STAL stall STAR Standard Termina...

Page 526: ...sition and altitude based upon current groundspeed VFOM Vertical Figure of Merit VFR Visual Flight Rules VHF Very High Frequency VI Heading Vector to Intercept VLOC VOR Localizer Receiver VM Heading V...

Page 527: ...Both LNAV VNAV and LPV approaches use the accuracy of WAAS to include vertical glide path guidance capability The additional accuracy and vertical guidance capability allows improved instrument appro...

Page 528: ...al en route portion of the ight plan remains active unless the instrument procedure is activated This may be done either when the procedure is loaded or at a later time Flight plans can also be stored...

Page 529: ...led i e no OBS or SUSP annunciation For automatic sequencing to occur the aircraft must also cross the bisector of the turn being navigated The bisector is a line passing through the waypoint common t...

Page 530: ...f 1 0 nm except under the following conditions When navigating with an active arrival route the ight phase and CDI scale will not change until the aircraft arrives at the rst waypoint in the arrive ro...

Page 531: ...ou want to discontinue the current approach appears The G1000 directs the pilot back to the transition waypoint and does not take into consideration any missed approach procedures if the current appro...

Page 532: ...Garmin G1000 Pilot s Guide for the Socata TBM 850 190 00709 00 Rev A D 6 APPENDIX D BLANK PAGE...

Page 533: ...n directional radio beacon VOR VOR DME VOR ILS VORTAC TACAN LINE SYMBOLS Item Symbol ICAO Control Area Class B Airspace Mode C Tower Area Warning Area Alert Area Caution Area Danger Area Prohibited Ar...

Page 534: ...Enabled User Waypoint Vertical Navigation Along Track Waypoint Parallel Track Waypoint Unanchored Flight Path Waypoint Top of Descent TOD Bottom of Descent BOD Navigating using Dead Reckoning STORMSCO...

Page 535: ...00 ft 100 ft Threshold Terrain Above Aircraft Altitude Terrain Color Terrain Location Red WARNING Terrain above or within 100 ft below the aircraft altitude Yellow CAUTION Terrain between 100 ft and 1...

Page 536: ...isplay enabled Stormscope display enabled NEXRAD display enabled Cloud Top display enabled Echo Top display enabled XM Lightning display enabled Cell Movement display enabled SIGMETs AIRMETs display e...

Page 537: ...lights 4 36 ANT BFO 4 27 Antenna stabilization 6 46 Antenna tilt 6 43 Approach D 2 Activating 5 104 5 105 ILS 7 43 Loading 5 73 5 102 5 104 Missed 7 45 Removing 5 105 WAAS 7 44 Approach Mode 7 28 7 43...

Page 538: ...Height DH 2 3 Declutter 1 24 Declutter display 2 36 Delete Flight Plans 5 77 Deleting an entire airway 5 78 5 79 Deleting an entire procedure 5 78 5 79 Deleting an individual waypoint 5 78 Deleting F...

Page 539: ...1347 1 1 1 15 1 42 GMU 44 1 1 Go Around Mode 7 22 7 45 7 46 Ground mapping 6 49 GRS 77 1 1 GTX 33 1 1 GTX 33 33D Transponder 4 29 H Heading 2 2 Heading Select Mode 7 25 HI SENS 4 24 Horizontal scan6 3...

Page 540: ...Night View 8 25 8 44 Non path descent 7 18 7 41 7 42 Normal operating mode 1 16 1 18 NO COMP A 3 O Obstacles A 10 A 12 OBS Mode 2 25 2 26 Oil engine Alerts 3 14 A 1 Pressure 3 3 3 5 Temperature 3 3 3...

Page 541: ...8 31 Terrain 1 24 6 67 A 10 A 20 Color indications E 3 Terrain Awareness and Warning System TAWS Annunciation 2 31 Tilt 6 42 6 43 Tilt line 6 43 Time system 1 34 TOD 5 134 5 135 5 141 Topographical da...

Page 542: ...5 49 VOR selection 4 16 VSI 5 136 Vspeeds 2 5 2 6 VS TGT 5 92 5 134 W WAAS 5 118 7 34 A 12 WAAS precision approach 7 44 Warranty i WATCH 6 47 6 48 Waypoint Automatic sequencing D 3 Skipping D 3 Waypoi...

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