Garmin G1000 Cockpit Reference Manual
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Garmin G1000 Cockpit Reference Manual

Integrated flight deck for socata tbm 850
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  • Page 1 Integrated Flight Deck Cockpit Reference Guide Socata TBM 850...
  • Page 3 SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE & AIRFRAME SYSTEMS NAV/COM/TRANSPONDER AUDIO PANEL AUTOMATIC FLIGHT CONTROL NAVIGATION FLIGHT PLANNING PROCEDURES HAZARD AVOIDANCE ADDITIONAL FEATURES ABNORMAL OPERATIONS ANNUNCIATIONS & ALERTS INDEX...
  • Page 5 Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to...
  • Page 6 WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications...
  • Page 7 Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit.
  • Page 8 NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and displays, are subject to change and may not reflect the most current G1000 system and aviation databases. Depictions of equipment may differ slightly from the actual equipment.
  • Page 9 RECORD OF REVISIONS Part Number Change Summary 190-00708-00 Initial Release Revision Date of Revision Affected Pages Description November, 2007 i through Index-4 Production Release 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 RR-1...
  • Page 10 RECORD OF REVISIONS Blank Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A RR-2...

  • Page 11: Table Of Contents

    5.8 Digital Clearance Recorder and Player ..... 5-3 2.10 Horizontal Situation Indicator (HSI)....2-9 Turn Rate Indicator and Heading Trend Vector .... 2-10 Course Pointer ............2-10 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 12 Load and Activate An Arrival Procedure......9-1 7.15 Nearest Airspaces..........7-30 9.2 Approaches .............. 9-2 Load and/or Activate an Approach Procedure....9-3 Activate An Approach in the Active Flight Plan ..... 9-3 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...
  • Page 13 Weather Mapping and Interpretation....... 10-21 GMU 44 Message Advisories........13-18 Operation in Weather Mode ........10-22 GDL 69A Message Advisories ........13-18 Ground Mapping and Interpretation ......10-29 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 14 GWX 68 Alert Messages.......... 13-18 GDC 74B Message Advisories........13-19 GCU 475 Message Advisories........13-19 GMC 710 Message Advisories ......... 13-20 Miscellaneous Message Advisories......13-20 INDEX ...................Index-1 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 15: Section 1: System Overview

    find AFCS Control Unit. operating instructions on the major features of the G1000 system more easily. It is not intended to be a NOTE: The pilot should read and thoroughly comprehensive operating guide. Complete operating understand the Socata TBM 850 Pilot’s Operating...

  • Page 16: Pfd Controls

    SECTION 1 SYSTEM OVERVIEW PFD CONTROLS Figure 1-1 PFD Controls Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...
  • Page 17 COM frequency field as a percentage. Press to ENT Key – Validates or confirms a menu turn the COM automatic squelch ON and OFF. selection or data entry. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 18: Controls Associated With The Mfd

    Pressing the FMS Knob characters with the FMS Knob. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 19: Afcs Controls

    NOTE: With the exception of the FD and SPD Mode. Keys, if a key is selected, its respective annuncia- tor is illuminated. Figure 1-3 AFCS Control Unit (GMC 710) 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 20 HSI of PFD1 when the VOR1, VOR2, or OBS/SUSP mode is selected. Pressing this knob centers the CDI on the currently selected VOR. The pilot-selected course provides course Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 21: Pfd Softkey Map

    Displays traffic information on Inset Map TOPO Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 22 Displays softkeys for selecting the #1 and #2 AHRS and Air Data Computers ADC1 Selects the #1 Air Data Computer ADC2 Selects the #2 Air Data Computer AHRS1 Selects the #1 AHRS AHRS2 Selects the #2 AHRS Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...
  • Page 23 Displays the HSI as an arc BRG2 Cycles the Bearing 2 Information Window through NAV2 or GPS/ , and ADF/ waypoint identifier and GPS-derived distance information frequency. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 24 Mode C replies, but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations. Automatically enters the VFR code (1200 in the U.S.A. only) CODE Displays transponder code selection softkeys 0-7 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 1-10...

  • Page 25: Mfd Softkey Map

    Displays a value of 50 feet in the RAD ALT window indicating the system is funcitoning correctly. ELEC Displays the Electrical Synoptics Page FUEL Displays the Fuel Synoptics Page Displays the General Synoptics Page for the anti-ice system and doors 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 1-11...

  • Page 26: Mfd

    1) Turn the large FMS Knob until the desired page group is selected. 2) Turn the small FMS Knob to select pages within the group. See Figure 1-10. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 27: Vertical Navigation

    Figure 1-10 Page Group Icon VERTICAL NAVIGATION When activating or loading an arrival or approach One of two altitude sources is used by the G1000 when giving vertical navigation guidance. WAAS GPS altitude is procedure into an active flight plan, the VNV ‘ALT’ fields used when giving guidance for a WAAS approach.
  • Page 28 Altitude Restriction • Altitudes displayed as a light blue subdued text Figure 1-11 VNV Altitudes cannot be used in the current vertical navigation calculations. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 1-14...

  • Page 29: Backlighting

    MFD: Updating the Jeppesen aviation database: 1) Press the MENU Key on the PFD to display the PFD 1) With the G1000 System OFF, insert the SD card Setup Menu window. containing the aviation database update into the 2) Press the small FMS Knob to activate the cursor.

  • Page 30: Garmin Databases

    MFD. prompt similar to the following is displayed: 2) Apply power to the G1000 System. View the MFD power-up splash screen. Check that the databases are initialized and displayed in the window of the splash screen.

  • Page 31: Pilot Profiles

    Press the ENT Key. The G1000 loads and displays profile. the system settings for the selected profile. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 1-17...

  • Page 32: Renaming A Profile

    In the ‘Delete Profile’ window, turn the FMS Knob to select the profile to be deleted. 6) Press the ENT Key. With ‘DELETE’ highlighted, press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 1-18...

  • Page 33: Section 2: Flight Instruments

    Course Deviation Indicator (CDI) Barometric Altimeter Setting Slip/Skid Indicator Horizontal Situation Indicator (HSI) Selected Altitude Bug Attitude Indicator Outside Air Temperature Vertical Speed Indicator (VSI) Figure 2-1 Default PFD Information 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 34 BRG1 Information Window Vertical Deviation/Glidepath/Glideslope Indicator Figure 2-2 Additional PFD Information Distance to Next Active Flight Plan Leg Bearing to Next Waypoint Waypoint Figure 2-3 PFD Navigation Status Box Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 35: Speed Indication

    Slip/Skid Indicator range. Refer to the Pilot’ s Operating Handbook (POH) for Aircraft Symbol Sky Representation speed criteria. Land Representation Roll Scale Zero Figure 2-6 Attitude Indicator 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 36: Altimeter

    6 seconds if the current rate of 1) Use the FMS Knob to select the AUX - System Setup vertical speed is maintained. Page on the MFD. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 37: Metric Display

    164 feet below the prescribed altitude at the FAF. The annunciation initially flashes. After a few seconds the flashing stops and the annunciation is displayed as shown in Figure 2-10. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 38: Vertical Deviation/Glidepath/Glideslope Indicator

    Figure 2-12 Glidepath Indicator The Glideslope Indicator appears when an ILS approach has been activated and an ILS is tuned in the active NAV receiver field (see Figure 2-13). Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 39: Marker Beacon Annunciations

    0 to 16,000 feet in 10-foot increments. The minimums are reset anytime the power is cycled. Altimeter Altitude Source Minimum Altitude Setting Figure 2-14 Marker Beacon Annunciations Figure 2-16 Barometric/Radar Minimum Descent Altitude Settings 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 40: Radar Altitude

    50 feet, indicating a properly functioning system. 3) Selecting the RA TEST Softkey again, or exiting the Figure 2-17 Barometric Minimum Descent Altitude System Page cancels the test. Alerting Visual Annunciations Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 41: Wind Data

    4) To remove the Wind Data Window, select the OFF Flight Phase Softkey. Turn Rate and Heading Trend Vector Heading Lubber Line Figure 2-20 Horizontal Situation Indicator 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 42: Turn Rate Indicator And Heading Trend Vector

    VNAV) course width, then 0.3 nm, points in the direction of the set course. depending on variables (see Figure Approach (LPV) 2-26) Missed Approach 0.3 nm Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 2-10...
  • Page 43 2 nm Landing Threshold CDI scale varies if Vectors-To-Final is activated Drawing not to scale Figure 2-26 Typical LNAV/VNAV and LPV Approach CDI Scaling 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 2-11...

  • Page 44: Bearing Pointers And Information Windows

    • DR – Navigating using Dead Reckoning due to an error in the GPS solution. Waypoint Identifier Bearing Pointer Source Icon Figure 2-29 BRG2 Information Window Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 2-12...

  • Page 45: Generic Timer

    3) Select the OBS Softkey again to disable OBS Mode. NOTE: The OBS Softkey is only displayed when navigating an active leg using GPS. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 2-13...
  • Page 46 SECTION 2 FLIGHT INSTRUMENTS Blank Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 2-14...

  • Page 47: Section 3: Engine & Airframe Systems

    Battery and Generator Currents Interturbine Temperature Selected Cabin Altitude Battery and Essential Bus Voltages Oil Pressure Oxygen Pressure Elevator, Aileron, and Rudder Trim and Flap Position Oil Temperature Fuel Quantity 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 48: Electrical System

    Standby Generator Battery Battery Bus Main Generator Main Bus Essential Bus Ground Power Unit Door Emergency Switch Power Buses Figure 3-3 Electrical Synoptics Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...
  • Page 49 Battery overheating is indicated in red with a ‘BAT OVHT’ annunciation; a CAS message is also generated. Figure 3-4 Cabin Leak Indication 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 50: Fuel System

    Left Fuel Tank Auxiliary Boost Pump Right Fuel Line Left Fuel Line Fuel Selector Fuel Flow Data Fuel Pressure Right Fuel Tank Figure 3-5 Fuel Synoptics Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...
  • Page 51 The aircraft’ s gross weight (GW) is entered on the AUX - Weight Planning Page (see the Flight Planning Section). A red “X” over a component indicates invalid data or a failed unit. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 52: General Systems

    Statuses of propeller, stall sensor heater, pitot probe, and windshield heat are also indicated on the diagram: • White indicates that heat is off (propeller and windshield) Figure 3-6 General Synoptics Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 53: Crew Alerting System (Cas)

    CAS messages are grouped by criticality (warning, until the issue is corrected. caution) and sorted by order of appearance (most recent messages on top). 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 54 Master Caution Indicator is also illuminated. Pressing the Master Caution Indicator acknowledges all flashing yellow messages, extinguishing the master caution lights, and stops caution message flashing. Messages are displayed until the issue is corrected. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...
  • Page 55 Vacuum pressure less than 3.75 in Hg * Only affected side (L, R, or L-R) displayed in CAS message; applicable messages listed here display L-R for example Table 3-4 Caution CAS Messages 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 56: Display Inhibits

    If a GEA or GIA fails, all CAS messages depending on sensors associated with that LRU are automatically inhibited. Inhibits cannot be activated by invalid sensor data. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 3-10...

  • Page 57: Section 4: Nav/Com And Transponder

    The NAV/COM controls and frequency boxes share the same locations on both Primary Flight Displays. NAV Frequency Box COM Frequency Box Controls Controls Figure 4-1 G1000 VHF NAV/COM Controls (PFD shown) 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 58 Frequency Transfer Key Dual NAV Dual COM Knob Knob • Turn to tune in desired frequencies. • Press to change tuning box positions. Figure 4-4 NAV/COM Controls Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 59: Radio Status Indications

    field if desired. Turn the small FMS Knob to adjust VOL/PUSH SQ Knob. the ADF volume to the desired level. Press the FMS Knob to exit all the fields. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 60: Dme Radio (Optional)

    Mode A and Mode C replies, but it does permit acquisition squitter and replies to discretely address Figure 4-10 Nearest Airports Window (PFD) Mode S interrogations. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 61: Reply Status

    Altitude Reporting) active. When entering a code, select the BKSP Softkey as needed to back up and change code Figure 4-14 Altitude Mode digits. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 62: Flight Id Reporting

    Figure 4-16 Timer/References Window 1) Select the TMR/REF Softkey to display the Timer/ References Window. 2) Turn the large FMS Knob to place the cursor in the Flight ID field. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 63: Section 5: Audio Panel

    (AUX unavailable) Digital Clearance Recorder Digital Clearance Recorder Play Key Pilot/Copilot Intercom Cabin Intercom VOL/SQ Volume/Squelch VOL Annunciation SQ Annunciation Reversionary Mode Figure 5-1 Audio Panel Controls 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 64: Com Radio Selection

    MUTE Key once when there is no marker indication present, or press twice when an indication is present. The key annunciator extinguishes when the marker beacon audio is turned off. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 65: Passenger Address System

    Powering off the unit automatically clears all recorded annunciator is lit when the cabin intercom is active on blocks. either audio panel. Figure 5-10 Recorder/Player Figure 5-8 Intcom Selection 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 66 If a COM input signal is detected while playing, play is halted and the new COM input signal is recorded as the latest block. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 67: Section 6: Automatic Flight Control

    NAV or APR Key press activates flight director. ***The selected navigation receiver must have a valid LOC signal before BC Key press activates flight director. Table 6-1 Flight Director Activation 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 68: Switching Flight Directors

    Figure 6-2 Flight Director Selection Indications selected flight director is also illuminated beside the XFR Key. When the flight directors are switched, the vertical and lateral modes revert to default. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 69: Command Bars

    The Command Bars are not displayed if attitude a cross pointer. information sent to the flight director is invalid or unavailable, pitch exceeds +30˚/-20˚, or bank exceeds Press the ENT Key. 65˚. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 70: Flight Director Modes

    • Go Around — Automatically disengages the flight director modes is invalid or unavailable. autopilot and commands a constant pitch angle and wings level while in the air Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...
  • Page 71 Altitude is to be captured instead of VNV Target Altitude ** ALTV armed automatically under VPTH when VNV Target Altitude is to be captured instead of Selected Altitude Table 6-2 Flight Director Vertical Modes 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 72 VNV Target Altitude) Pitch Hold Mode Active Selected Altitude Capture Mode Armed Selected Altitude Command Bars Maintain Desired Pitch Reference Figure 6-7 Pitch Hold Mode Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...
  • Page 73 To adjust the Altitude Reference in this case, the CWS Altitude Capture Mode does not cancel the mode. Button must be pressed again after the Selected Altitude is reached. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 74 Mode Armed Reference Selected Altitude Vertical Speed Reference Vertical Speed Reference Bug Command Bars Indicate Climb to Attain Vertical Speed Reference Figure 6-9 Vertical Speed Hold Mode Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...
  • Page 75 Selected Altitude. Flight Level Change Airspeed Selected Altitude Capture Mode Active Reference Mode Armed Airspeed Reference Airspeed Reference Figure 6-10 Flight Level Change Mode (IAS) 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 76 The required within five minutes of descent path interception Command Bars provide vertical profile guidance based on specified altitudes (entered manually or loaded from the Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-10...
  • Page 77 Selected Altitude Below VNV Target Vertical Deviation Indicator Required Vertical Speed Bug Enroute Phase of GPS is Selected Flight Navigation Source Figure 6-12 Vertical Path Capture 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-11...
  • Page 78 Deviation Indicator is removed from the PFD). • A display enters Reversionary Mode (this does not apply to an active vertical direct-to). Figure 6-14 Flight Level Change VNV Non-Path Descent Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-12...
  • Page 79 flight plan (see the Navigation section for details). Target Altitude is shown as the Altitude Reference beside the ‘ALTV’ annunciation and remains displayed above the 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-13...
  • Page 80 GPS Approach Mode Active Glidepath Mode Active Glidepath Indicator Command Bars Indicate Descent on Glidepath GPS is Selected Naviga- Approach tion Source Active Figure 6-16 Glidepath Mode Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-14...
  • Page 81 Glideslope Mode Active Active ILS Frequency Tuned Glideslope Indicator Command Bars Indicate Descent on Localizer/Glides- lope Path NAV2 (localizer) is Selected Navigation Source Figure 6-18 Glideslope Mode 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-15...

  • Page 82: Lateral Modes

    Go Around Mode Active Autopilot Disconnect Annunciation Flashes Yellow 5 sec Command Bars Indicate Climb Figure 6-20 Go Around Mode Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-16...
  • Page 83 * No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in green along the Roll Scale of the Attitude Indicator. Table 6-3 Flight Director Lateral Modes 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-17...
  • Page 84 Table 6-4 Roll Hold Mode Responses Changing the Roll Reference The roll reference can be changed by pressing the CWS Button, establishing the desired bank angle, then releasing the CWS Button. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-18...
  • Page 85 CWS Button. Heading Select Mode Active Pitch Hold Mode Active Command Bars Track Selected Heading Selected Heading Selected Heading Figure 6-23 Heading Select Mode 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-19...
  • Page 86 Pitch Hold Mode Active Command Bars Indicate Left Turn to Track GPS Course and Climb to Intercept Selected Altitude GPS is Selected Navi- gation Source Figure 6-24 Navigation Mode Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-20...
  • Page 87 (annunciated in white to the left of the active lateral 105°. mode). VOR Approach Mode (VAPP) provides greater sensitivity for signal tracking than VOR Navigation Mode. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-21...
  • Page 88 • Approach Mode is active and Navigation source is manually switched • GPS Navigation Mode is active and the FAF is crossed after the automatic navigation source switch from GPS to LOC Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-22...
  • Page 89 The flight director creates roll steering commands from the Selected Course and deviation when in Backcourse Mode. Backcourse Mode Active Glideslope Mode Active LOC2 is Selected Navigation Source Figure 6-27 Backcourse Mode 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-23...

  • Page 90: Autopilot And Yaw Damper Operation

    This allows the aircraft to be trimmed using a control wheel switch rather than the trim wheel. Manual trim commands Figure 6-28 Autopilot and Yaw Damper Engaged Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-24...

  • Page 91: Control Wheel Steering

    ‘AP’ annunciation and a three-second autopi- lot disconnect aural alert. The AP DISC or MEPT ARM Switch may be used to cancel the aural alert. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-25...

  • Page 92: Procedures

    ILS approach for runway 35L and LPV (WAAS) approach for runway 35R are shown and a missed approach is executed. KCOS KMKC Figure 6-33 Flight Plan Overview Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-26...
  • Page 93 ‘ALT’ annunciation flashes for up to 10 seconds; the autopilot transitions to Altitude Hold Mode and levels the aircraft. Selected Altitude of 12,000 MSL ALT Mode KMKC Figure 6-34 Departure 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-27...

  • Page 94: Intercepting A Vor Radial

    Course to 255°. Note that at this point, the flight director is still in Heading Select Mode and the autopilot continues to fly 290°. Figure 6-35 Intercepting a VOR Radial Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-28...

  • Page 95: Flying A Flight Plan/Gps Course

    Press the NAV Key to activate GPS Navigation Mode. The autopilot guides the aircraft along the active flight plan leg. Salina (SLN) Hays (HYS) Figure 6-36 Transition to GPS Flight Plan 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-29...

  • Page 96: Descent

    Mode and levels the aircraft. to 10,000 feet. Cruise Altitude of 12,000 MSL ALT Mode Selected Altitude of 10,000 MSL ALT Mode Figure 6-37 FLC Descent Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-30...
  • Page 97 ALT Mode VNAV Target Altitude of 10,000 MSL Selected Altitude (set below VNAV Target Altitude) Along-track Offset, 3 nm before OPSHN 3 nm Figure 6-38 VPTH Descent 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-31...
  • Page 98 ALT Mode ALT Mode Selected Altitude of 9,400 MSL ALT Mode VNAV Target Altitude of 9,000 MSL Selected Altitude OPSHN HABUK 3 nm Figure 6-39 Non-path Descent Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-32...

  • Page 99: Approach

    flies the ILS approach: • Push the AP DISC Switch at the decision height and land the aircraft. • Use the GA Switch to execute a missed approach. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-33...
  • Page 100 • Push the AP DISC Switch at the Decision height and land the aircraft. • Use the GA Switch to execute a missed approach. Figure 6-41 LPV Approach to KCOS Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-34...

  • Page 101: Go Around/Missed Approach

    Selected Altitude Capture Mode, indicated by the green ‘ALTS’ annunciation flashing for up to 10 seconds. Figure 6-42 Go Around/Missed Approach (GPS 35R KCOS 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-35...

  • Page 102: Afcs Annunciations And Alerts

    Power must be cycled to the servos to remedy the situation. Preflight system test failed; aural alert sounds at failure Table 6-4 AFCS Status Alerts Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-36...

  • Page 103: Overspeed Protection

    Engine power should be reduced as pitch is adjusted by the autopilot to slow the aircraft. The annunciation disappears when the overspeed condition is resolved. Airspeed Indicator Figure 6-44 Overspeed Annunciation 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 6-37...
  • Page 104 SECTION 6 – AUTOMATIC FLIGHT CONTROL Blank Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 6-38...

  • Page 105: Section 7: Navigation

    7) Press the ENT Key. The option to select ‘MSL’ or ‘AGL ‘is now displayed. 8) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’. Figure 7-1 Navigation Map Page (Enroute) 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 106 flight plan waypoint list is displayed as in Figure ‘ACTIVATE?’. 7-3. The list is populated only when navigating a 5) Press ENT again to activate a Direct-to. flight plan. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 107: Direct-To Navigation From The Pfd

    3) With ‘Cancel Direct-To NAV’ highlighted, press the 5) Press the ENT Key. The cursor is now displayed on ENT Key. If a flight plan is still active, the G1000 ‘ACTIVATE?’. resumes navigating the flight plan along the closest 6) Press ENT again to activate a Direct-to.
  • Page 108 Figure 7-9 Nearest Airport List (PFD) 3) Turn the small FMS Knob to the right to display the ‘NRST’ airports to the aircraft’s current position as shown in Figure 7-9. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 109: Navigating An Example Flight Plan

    2) Press the MENU Key to display the Options Window. After takeoff, ATC assigns a heading of 240º. The cursor flashes on ‘Cancel Direct-to NAV’. 3) Press the ENT Key to cancel the direct-to. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 110 CDI flight phase displayed on the HSI indicating 1.0 to heading 290° as seen in Figure 7-12. nm CDI scaling. Figure 7-12 Assigned Heading of 290º Figure 7-11 Assigned Heading of 240º Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...
  • Page 111 Press the ENT Key. TOP is now inserted into the flight plan as in Figure 7-15. Figure 7-13 Begin Adding V4 to the Flight Plan Figure 7-15 TOP Inserted into the Flight Plan 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 112 Press the ENT Key. The list of available exits for V4 is now displayed as in Figure 7-17. Figure 7-18 Ready to Load V4 k) Press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...
  • Page 113 V4 is now the active flight disappears from the HSI and the CDI is positioned plan leg. Note also, the crosstrack (XTK) distance 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 114 9) As seen in Figure 7-24,V244 is now the active flight plan leg. Figure 7-24 V244 Now Active Leg Figure 7-22 Turn on to Active Leg Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 7-10...
  • Page 115 Window is now displayed as shown in Figure 7- Figure 7-27 Enter VNV Altitude e) An altitude of 10,000 feet is entered as requested by ATC. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-11...
  • Page 116 Note the Direct-to waypoint is within the loaded arrival procedure, therefore, phase of flight scaling for the CDI changes to Terminal Mode and is annunciated by displaying ‘TERM’ on the HSI. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 7-12...
  • Page 117 Turn either FMS Knob to select the desired transition. In this case, the Initial Approach Fix (IAF) at HABUK is used. g) Press the ENT Key. Figure 7-31 List of Available Approaches 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-13...
  • Page 118 The altitude values must be designated for use by the pilot if they are to be used in computing vertical guidance. a) Press the FMS Knob to activate the cursor. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 7-14...
  • Page 119 The default Flight Path Angle (FPA) is -3.0 degrees and a required vertical speed is computed to maintain the -3.0 FPA. To change the vertical flight path, perform the following steps. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-15...
  • Page 120 (VDI) Vertical Speed Indicator Figure 7-37 Adjusting the Descent (RVSI) c) Press the ENT Key. Figure 7-39 VDI & RVSI Upon Reaching Top of Descent (TOD) Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 7-16...
  • Page 121 OPSHN, the aircraft will be at 10,000 feet. Figure 7-42 Turn to intercept OPSHN to FSHER Leg Figure 7-41 Approaching Bottom of Descent (BOD) at OPSHN Offset Waypoint 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-17...
  • Page 122 Note the TOD point on the map. Annunciations for the upcoming turn and descent, as well as the VDI and RVSI, appear on the PFD as the flight progresses. Figure 7-44 Approaching PYNON Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 7-18...
  • Page 123 Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’ as shown in Figure 7-46. Figure 7-47 Descending Turn to the Initial Approach Fix (IAF) Figure 7-46 Manually Activate Approach 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-19...
  • Page 124 ABOVE” 6,370 feet at the Missed Approach Point (MAP) (RW35R) as seen in Figure 7-49. Figure 7-48 Descending to the FAF Figure 7-49 Descending to the Missed Approach Point Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 7-20...
  • Page 125 MAP. Select the SUSP Softkey on the PFD to resume automatic waypoint sequencing through the missed approach procedure. Figure 7-50 Missed Approach Active 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-21...
  • Page 126 Figure 7- established at the MAHP (MOGAL) as shown in Figure 7-51. Figure 7-52 Hold Established Figure 7-51 Establishing the Holding Pattern Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 7-22...

  • Page 127: Airport Information

    3) Turn the small FMS Knob to the right to display the 2) Enter the desired airport identifier. ‘NRST’ airports to the aircraft’s current position as shown in Figure 7-55. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-23...
  • Page 128 5) To remove the cursor, press the FMS Knob . 3) Enter the desired facility name or city. 4) Press the ENT Key. 5) To remove the flashing cursor, press the FMS Knob . Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 7-24...

  • Page 129: Intersection Information

    ENT Key. If there are duplicate identifiers in the cursor. database, a list is displayed from which to choose the desired location. 4) Press the FMS Knob to remove the flashing cursor. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-25...

  • Page 130: Vor Information

    ENT Key to place the frequency in the NAV receiver standby field. 5) Press the FMS Knob to remove the flashing cursor. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 7-26...

  • Page 131: Nearest Airports Information On The Pfd

    field. 3) Press the Frequency Transfer Key to make the 5) Press the FMS Knob to remove the flashing frequency the active frequency. cursor. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-27...

  • Page 132: Nearest Intersections

    Page pertains to the selected NDB. 3) Press the FMS Knob to remove the flashing 3) Press the FMS Knob to remove the flashing cursor. cursor. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 7-28...

  • Page 133: Nearest Vor

    1) With the Nearest VOR Page displayed, select the nm, these are displayed with the closest listed FREQ Softkey to highlight the VOR frequency in the first. ‘FREQUENCY’ field. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-29...

  • Page 134: Nearest Frequencies

    ARTCC, FSS, or WX Softkey to place the cursor • If the aircraft is within two nautical miles of an in the appropriate field. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 7-30...
  • Page 135 3) Press the ENT Key to load the frequency into the COM frequency standby field. 4) Press the FMS Knob to remove the flashing cursor. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 7-31...
  • Page 136 SECTION 7 – NAVIGATION Blank Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 7-32...

  • Page 137: Section 8: Flight Planning

    NEW Softkey. A waypoint is created at the current aircraft position. 2) Turn the small FMS Knob to enter first character of the waypoint name. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 138: Create User Waypoints From The Navigation Map Page

    3) Turn the large FMS Knob to highlight the desired flight plan and select the ACTIVE Softkey. 4) With ‘OK’ highlighted, press the ENT Key to activate the flight plan. To cancel the flight plan activation, Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 139: Activate A Flight Plan Leg

    2) Press the MENU Key to display the Page Menu window. Figure 8-8 Invert Flight Plan Figure 8-9 Invert Flight Plan Confirmation Figure 8-6 Delete Flight Plan 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 140: Create A New Flight Plan

    8) When all waypoints have been entered, press the FMS Knob to return to the Flight Plan Catalog Page. The new flight plan is now in the list. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 141: Enter An Airway In A Flight Plan

    Figure 8-16 Enter Airway Identifier 7) Select the LD AIRWY Softkey. A list of available airways is now displayed. Figure 8-14 Load Airway Entry Point 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 142: Load A Departure

    11) With the desired exit point highlighted, press the With ‘OK’ highlighted, press the ENT Key to remove ENT Key. the selected procedure or airway. 12) With ‘LOAD?’ highlighted, press the ENT Key. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 143: Store A Flight Plan

    FMS Knob to activate the to be copied. cursor. 3) Select the COPY Softkey. 2) Turn the large FMS Knob to select the waypoint to be deleted. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 144: Delete A Flight Plan

    LD WPT Softkey. 3) Press the ENT Key to confirm the entry. 6) To change the user waypoint name, follow the procedure for modifying a user waypoint. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 145: Enter A Pilot And Stores Weight

    3) Press the ENT Key to confirm the entry. The ‘ZERO FUEL WEIGHT’ is calculated by adding the basic empty, pilot and stores, passenger, and cargo weights. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 146: Weight Caution And Warning Conditions

    Again, turn the FMS Knobs to enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint. Or : Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 8-10...
  • Page 147 Press the ENT Key when finished. 9) The flashing cursor moves to the calibrated airspeed field. Turn the FMS Knobs to enter a calibrated airspeed. Press the ENT Key when finished. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 8-11...
  • Page 148 SECTION 8 – FLIGHT PLANNING Blank Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 8-12...

  • Page 149: Section 9: Procedures

    8) A list of available transitions is displayed for the departure. Turn either FMS Knob to highlight the Figure 9-3 Select Arrival desired transition waypoint and press the ENT Key. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...

  • Page 150: Approaches

    flight plan. L/VNAV GPS approach using published LNAV/VNAV minima. GPS approach using published LPV minima. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 151: Load And/Or Activate An Approach Procedure

    2) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’. 3) Press the ENT Key. The approach procedure is now active and a direct-to is initiated to the IAF. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850...
  • Page 152 SECTION 9 – PROCEDURES Blank Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A...

  • Page 153: Section 10: Hazard Avoidance

    Strike is between 6 and 60 seconds old Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Figure 10-3 Map Setup Group List 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-1...

  • Page 154: Stormscope Page

    360˚ viewing area or select the ARC Softkey to display a 120˚ viewing area. 2) Turn the small FMS Knob until the Stormscope Page is selected. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-2...

  • Page 155: Xm Weather (Optional)

    Map Page. METAR Text Text Softkey Figure 10-8 METAR and TAF Text Displayed on the Airport (Weather) Information Page Figure 10-7 Navigation Map Page Displaying NEXRAD Weather 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-3...

  • Page 156: Displaying Weather On The Weather Data Link Page

    2 kilometer radius of the actual strike location. Therefore, the exact location of shown in grayish-purple. The display is updated the strike is not displayed. every five minutes. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-4...

  • Page 157: Map Panning Information - Weather Data Link Page

    • Surface Analysis and Flood conditions provided by the National • Freezing Levels Weather Service (NWS). The display is updated • Winds Aloft every 5 minutes. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-5...

  • Page 158: Weather Product Age

    Surface Analysis time, the product time changes from light blue to amber in TFRs color. Winds Aloft TAFs Clouds Tops Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-6...

  • Page 159: Traffic Advisory System (Tas)

    Traffic Mode field. 6) Rotate the Joystick clockwise to display a larger area or rotate counter-clockwise to display a smaller area. Figure 10-11 Self Test OK Display 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-7...

  • Page 160: Displaying Traffic On The Navigation Map

    2) Select the TRAFFIC Softkey. Traffic is now displayed on the map. Non-Bearing Traffic Off Scale Traffic Advisories Banner Figure 10-13 TAS Traffic on Navigation Map Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-8...

  • Page 161: Terrain And Obstacle Proximity

    (Height is less than (Height is less than (Height is greater than (Height is greater than 1000’ AGL) 1000’ AGL) 1000’ AGL) 1000’ AGL) Figure 10-15 Obstacle Symbols 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-9...

  • Page 162: Displaying Terrain And Obstacles On The Navigation

    Select the 360 Softkey to return to the 360° default display. 4) Rotate the Joystick clockwise to display a larger area or rotate counter-clockwise to display a smaller area. Figure 10-17 TAWS Page (ARC View) Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-10...

  • Page 163: Enable/Disable Aviation Data

    Enable TAWS: If TAWS has been inhibited, from the TAWS Page select the INHIBIT Softkey. The ‘TAWS INHB” annunciation is removed. Figure 10-18 TAWS Page Menu 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-11...

  • Page 164: Manual System Test

    When an RTC or ROC alert is issued, a potential impact point is displayed on the TAWS Page as a yellow or red ‘X’. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-12...

  • Page 165: Excessive Descent Rate Alert (Edr)

    1500 "PULL UP" "PULL UP" message. 1000 2000 4000 6000 8000 10000 12000 Descent Rate Figure 10-20 Excessive Descent Rate 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-13...

  • Page 166: Displaying Terrain And Obstacles On The Navigation

    Figure 10-23 Alert Pop-Up Press the ENT Key to display the TAWS Page, or press the CLR Key to remain on the Navigation Map Page. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-14...

  • Page 167: Taws Alerts Summary

    “Too Low, Terrain” Altitude Callout “500” None None “Five-Hundred” Excessive Descent Rate Caution (EDR) “Sink Rate” Negative Climb Rate Caution (NCR) “Don’t Sink” “Too Low, Terrain” 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-15...

  • Page 168: Alert Annunciations

    None “TAWS System Test OK” Alert Annunciations Alert Annunciation Figure 10-25 Alert Annunciation on the PFD Alert Annuciation Figure 10-24 Alert Annunciation on the TAWS Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-16...

  • Page 169: Airborne Color Weather Radar

    18,000 ft. Range (nautical miles) Figure 10-26 Radar Beam from 10 inch Antenna 320 nm Figure 10-27 Radar Beam in Relation to the Curvature of the Earth 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-17...
  • Page 170 Areas in question appear as ‘shadowed’ or gray area on the radar display. Proper use of the antenna tilt control can also help detect radar shadows. Figure 10-28 Precipitation Type and Reflectivity Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-18...
  • Page 171 A large incident angle gives the radar system a smaller detectable range and lower display intensity due to minimized reflection of the radar energy. Figure 10-29 Angle of Incidence 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-19...
  • Page 172 +4° +3° 1000 +2° +1° 0° -1° 1000 -2° -3° -4° 2000 3000 4000 10 nm Figure 10-31 Vertical Change in Radar Beam per Nautical Mile Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-20...

  • Page 173: Weather Mapping And Interpretation

    Vertical scanning and antenna tilt management may be necessary to identify areas of maximum intensity. Figure 10-34 The ‘Blind Alley’ - Illustration 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-21...

  • Page 174: Operation In Weather Mode

    When transmitting while the Figure 10-35 Horizontal Scan Display aircraft is on the ground, no personnel or objects should be within 11 feet of the antenna. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-22...
  • Page 175 5) Turn the Joystick to select the desired map range. 6) The horizontal scan is initially displayed (Figure 10-35). If desired, select the VERTICAL Softkey to change to vertical scanning. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-23...
  • Page 176 Line on the desired storm cell or other area to be vertically scanned. Scan Line Bearing Line Figure 10-38 Vertical Scan Display Figure 10-37 Bearing Line on Horizontal Scan Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-24...
  • Page 177 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 Joystick can also be used to adjust tilt. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-25...
  • Page 178 If the Bearing Line is not displayed, press the MENU Key and turn the large FMS Knob to select ‘Show Bearing Line’. Press the ENT Key. Figure 10-40 Manual Gain Set Below Calibrated Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-26...
  • Page 179 2) Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softkey to deactivate. The current stabilization condition is shown in the upper right of the weather radar display. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-27...
  • Page 180 To avoid this issue, set the display range to less than 80 nm in the terminal area. Weather alerts can also be deactivated in the terminal area. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-28...

  • Page 181: Ground Mapping And Interpretation

    7) Press the FMS Knob to remove the cursor. verifying aircraft position. A “picture” of the ground is represented much like a topographical map that can be 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 10-29...
  • Page 182 SECTION 10 – HAZARD AVOIDANCE Blank Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 10-30...

  • Page 183: Section 11: Additional Features

    2) Turn the large FMS Knob to highlight the Map Setup Menu Option and press the ENT Key. Figure 11-2 Navigation Map PAGE MENU, Map Setup Option Figure 11-1 SafeTaxi Depiction on the Navigation Map Page 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 11-1...
  • Page 184 7) Press the ENT Key to complete the selection. 8) Press the FMS Knob to return to the Navigation Map Page. SafeTaxi Option SafeTaxi Display Range Options Figure 11-4 SafeTaxi Display Range Options Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 11-2...

  • Page 185: Terminal Procedure Charts (Optional)

    PLAN PROFILE MINIMUMS Selecting the BACK Softkey returns These softkeys are only available with the ChartView option. to the Chart Selection Softkeys. Figure 11-5 ChartView Softkeys 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 11-3...

  • Page 186: Chart Options

    Aircraft Not Shown Icon appears (Fig- ure 11-7). If the Chart Scale Box displays a banner CHART NOT TO SCALE, the aircraft symbol is not shown. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 11-4...
  • Page 187 Selecting the PROFILE Softkey displays the approach chart descent profile strip. Figure 11-8 Header View Selecting the PLAN Softkey shows the approach chart two dimensional plan view. Figure 11-10 Profile View 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 11-5...

  • Page 188: Day/Night View Selection

    2) Turn the large FMS Knob to highlight the Chart setting to become active. This may be accomplished Setup Menu Option, then press the ENT Key. by selecting another page or changing the display range. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 11-6...

  • Page 189: Xm Radio (Optional)

    2) Select the Auxiliary Page Group. 3) Select the next to last page in the AUX Page Group. 4) If necessary, select the INFO Softkey to display the XM Information Page. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 11-7...

  • Page 190: Using Xm Radio

    1) Select the CATGRY Softkey on the XM Radio Page. Categories Field 2) Select the CAT + and CAT - Softkeys to cycle Figure 11-15 XM Radio Page through the categories. Or : Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 11-8...
  • Page 191 Access the Preset Channels Softkeys Select MORE to Cycle Through the Preset Select SET to Channels Save Each Preset Channel Figure 11-17 Accessing and Selecting XM Preset Channels 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 11-9...

  • Page 192: Data Link Receiver Error Messages

    WEATHER DATA LINK FAILURE Weather Datalink Page - center of page within last 5 minutes ACTIVATION REQUIRED Weather Datalink Page - center of page XM subscription is not activated Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 11-10...

  • Page 193: Scheduler

    4) Use the FMS Knob to enter the message text to be displayed in the Alerts Window and press the ENT Key. Figure 11-19 Scheduler (Utility Page) 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 11-11...

  • Page 194: Deleting A Scheduler Message

    The softkey revers to the ALERTS label and when selected, the Alerts Window is removed from the display and the scheduler message is deleted from the message queue. Figure 11-20 PFD Alerts Window Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 11-12...

  • Page 195: Section 12: Abnormal Operation

    2) MFD – By pressing the DISPLAY BACKUP button on the left or the right audio panel. PFD1 PFD2 Normal Operation Figure 12-1 G1000 Reversionary Mode: Failed PFD1 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 12-1...

  • Page 196: Unusual Attitudes

    GPS-derived position data is restored. While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position, the system automatically reverts Figure 12-2 Extreme Pitch Indication to Dead Reckoning (DR) Mode.
  • Page 197 As a result of operating in DR Mode, all GPS-derived data is computed based upon an estimated position and is DR Mode is indicated on the G1000 by the appearance displayed as yellow text on the display to denote degraded of the letters ‘DR’...
  • Page 198 SECTION 12 – ABNORMAL OPERATION Blank Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 12-4...

  • Page 199: Section 13: Annunciations & Alerts

    OIL PRESS Oil pressure below 60 psi OXYGEN Oxygen cylinder closed PARK BRAKE Parking brake applied Torque greater than or equal to 124.5% maximum torque TORQUE 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 13-1...

  • Page 200: Caution Messages

    Specified pitot heat (left or right) off PROP DEICE FAIL Prop deice selected and not on PROP DEICE ON Prop deice on while engine off REAR CARGO DOOR Rear cargo door open Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 13-2...

  • Page 201: Comparator Annunciations

    No data from one or both heading sensors. PIT NO COMP No data from one or both pitch sensors. ROLL NO COMP No data from one or both roll sensors.. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 13-3...

  • Page 202: Reversionary Sensor Annunciations

    “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up” Imminent Obstacle Impact Warning (IOI) “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up” “Obstacle, Obstacle; Pull Up, Pull Up” Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 13-4...

  • Page 203: Taws System Status Annunciations

    “TAWS Available” will be heard when sufficient GPS signal is re-established. System Test in progress None None System Test pass None None “TAWS System Test OK” 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 13-5...

  • Page 204: Other G1000 Aural Alerts

    Figure 13-1 G1000 System Messages This section describes various G1000 system message advisories. Certain messages are issued due to an LRU or an LRU function failure. When a message is issued, the MSG Softkey flashes. Selecting the MSG Softkey to view the message in the Message Window.
  • Page 205 Figure 13-2 G1000 System Failure Annunciations System Annunciation Comment Attitude and Heading Reference System is aligning. Display system is not receiving attitude information from the AHRS. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 13-7...
  • Page 206 When ‘LOI’ is displayed, GPS information is either not present or is invalid for navigation use. Note that AHRS utilizes GPS inputs during normal operation. AHRS operation may be degraded if GPS signals are not present (see POH). Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 13-8...

  • Page 207: Mfd & Pfd Message Advisories

    Recheck settings. The pilot may reconfigure the MFD & PFDs with preferred settings, if desired. XTALK ERROR – A flight display The MFD and PFDs are not communicating with each other. The G1000 system crosstalk error has occurred. should be serviced.

  • Page 208: Database Message Advisories

    A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by PFD2 KEYSTK – PFD2 [key name] Key pressing it several times. The G1000 system should be serviced if the problem is stuck. persists.
  • Page 209 The MFD and/or PFD detected a failure in the obstacle database. Ensure that the PFD1 DB ERR – PFD1 obstacle data card is properly inserted. Replace data card. If problem persists, The G1000 database error exists. system should be serviced.
  • Page 210 The MFD and/or PFD detected a failure in the Safe Taxi database. Ensure that the PFD1 DB ERR – PFD1 Safe Taxi data card is properly inserted. Replace data card. If problem persists, The G1000 database error exists. system should be serviced.

  • Page 211: Gma 1347D Message Advisories

    The audio panel self-test has detected a problem in the unit. Certain audio functions service. Return unit for repair. may still be available, and the audio panel may still be usable. The G1000 system GMA2 SERVICE – GMA2 needs should be serviced when possible.

  • Page 212: Gia 63W Message Advisories

    GIA1 SERVICE – GIA1 needs service. Return the unit for repair. The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000 system should be serviced. GIA2 SERVICE – GIA2 needs service. Return the unit for repair.
  • Page 213 COM1 TEMP – COM1 over temp. The system has detected an over temperature condition in COM1 and/or COM2. Reducing transmitter power. The transmitter is operating at reduced power. If the problem persists, the G1000 COM2 TEMP – COM2 over temp. system should be serviced.

  • Page 214: Gea 71 Message Advisories

    The GEA2 configuration settings do not match those of backup configuration Config service req’d. memory. The G1000 system should be serviced. MANIFEST – GEA1 software The #1 GEA 71 has incorrect software installed. The G1000 system should be mismatch, communication halted. serviced. MANIFEST – GEA2 software The #2 GEA 71 has incorrect software installed.

  • Page 215: Gtx 33 & Gtx 33D Message Advisories

    AHRS1 TAS – AHRS1 not receiving The #1 AHRS is not receiving true airspeed from the air data computer. The AHRS airspeed. relies on GPS information to augment the lack of airspeed. The G1000 system should be serviced. AHRS2 TAS – AHRS2 not receiving The #2 AHRS is not receiving true airspeed from the air data computer.

  • Page 216: Gmu 44 Message Advisories

    GRS 77 Message Advisories (Cont.) Message Comments AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving backup GPS information. The G1000 system should backup GPS information. be serviced. AHRS2 GPS – AHRS2 not receiving The #2 AHRS is not receiving backup GPS information. The G1000 system should backup GPS information.

  • Page 217: Gdl 69A Message Advisories

    A failure has been detected in the GDL 69. The receiver is unavailable. The G1000 system should be serviced MANIFEST – GDL software mismatch, The GDL 69 has incorrect software installed. The G1000 system should be communication halted. serviced. GWX 68 Alert Messages...

  • Page 218: Gcu 475 Message Advisories

    A key is stuck on the GMC 710 bezel. Attempt to free the stuck key by pressing is stuck. it several times. The G1000 system should be serviced if the problem persists. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.

  • Page 219: Miscellaneous Message Advisories

    Message Comments FPL WPT LOCK – Flight plan waypoint Upon power-up, the G1000 system detects that a stored flight plan waypoint is is locked. locked. This occurs when an aviation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message.
  • Page 220 -[xxxx] position with alternate navigation sources. TRAFFIC FAIL – Traffic device has The G1000 is no longer receiving data from the traffic system. The traffic device failed. should be serviced. Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.
  • Page 221 CRUISE II – Cruise II conditions met. Cruise II engine trend data log has been captured. EXCEEDANCE – Engine exceedance An engine exceedance log has been captured. data is being logged. 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 13-23...
  • Page 222 SECTION 13 – ANNUNCIATIONS & ALERTS Blank Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A 13-24...
  • Page 223 Cabin pressure altitude 3-1 Dual CDU failure 12-1 WAAS 6-34 Warning 3-8, 13-1 Approaches 9-2 Cargo 8-9 Approach activation 4-4 CAS Messages 13-1 Category 11-8 ECHO TOPS 10-4 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Index-1...
  • Page 224 Lightning 10-2, 10-3, 10-4 Glidepath Mode 6-14, 6-21 Navigation Mode 6-20–6-21, 6-28–6- LNAV 2-6, 7-5 Glidepath Mode (GP) 6-34 Load approach 8-6 Glideslope 2-6, 7-20 Navigation Status Box 2-1 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A Index-2...
  • Page 225 Preset channels 11-9 Stormscope lightning data 10-2, 10-3 Procedures Strike 10-2 GFC 700 6-26–6-37 Strike mode 10-2 Propeller speed 3-1 System message advisories 13-6 System time 2-1 190-00708-00 Rev. A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Index-3...
  • Page 226 XM weather 10-3, 10-4 VDI 7-16, 7-17 XPDR softkey 4-4, 4-5, 4-6 Vertical Descent Indicator 7-16 Vertical Deviation 2-6 Vertical deviation 6-11 Vertical deviation guidance 1-14 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev. A Index-4...
  • Page 228 Liberty House, Bulls Copse Road Hounsdown Business Park Southampton, SO40 9RB, U.K. p: 44/0870.8501241 f: 44/0870.8501251 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com 190-00708-00 Rev. A © 2007 Garmin Ltd. or its subsidiaries...

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