Integrated Flight Deck Cockpit Reference Guide Socata TBM 850
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
Copyright © 2007 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0719.00 or later for the Socata TBM 850. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.
WARNINGS, CAUTIONS, & NOTES 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 requiring a certified terrain awareness system.
WARNINGS, CAUTIONS, & NOTES WARNING: The Garmin G1000, as installed in the Socata TBM 850 aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000.
WARNINGS, CAUTIONS, & NOTES CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode.
RECORD OF REVISIONS Part Number 190-00708-00 Change Summary Initial Release Revision Date of Revision Affected Pages A November, 2007 i through Index-4 190-00708-00 Rev.
RECORD OF REVISIONS Blank Page RR-2 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.
TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW.................................... 1-1 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 PFD Controls ............................................................ 1-2 Controls Associated With the MFD ..................... 1-4 AFCS Controls .......................................................... 1-5 PFD Softkey Map .................................................... 1-7 MFD Softkey Map ................................................. 1-11 MFD Page Groups ................
TABLE OF CONTENTS SECTION 6: AUTOMATIC FLIGHT CONTROL ............. 6-1 6.1 6.2 6.3 6.4 Flight Director Activation ..................................... 6-1 Switching Flight Directors .................................... 6-2 Command Bars ........................................................ 6-3 Flight Director Modes............................................ 6-4 Vertical Modes ............................................................ 6-4 Lateral Modes ................................................
TABLE OF CONTENTS SECTION 10: HAZARD AVOIDANCE ........................... 10-1 10.1 Customizing the Hazard Displays on the Navigation Map .................................................... 10-1 10.2 STORMSCOPE® (Optional) ................................... 10-1 Displaying Stormscope Lightning Data on the Navigation Map Page ................................................ 10-1 Stormscope Page....................................................... 10-2 10.3 XM Weather (Optional) .........................
TABLE OF CONTENTS 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 ...................................................................................
SECTION 1 SYSTEM OVERVIEW SECTION 1: SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide. Complete operating procedures for the complete system are found in the G1000 Pilot’s Guide for the Socata TBM 850 (190-0070900): 190-00708-00 Rev.
SECTION 1 SYSTEM OVERVIEW 1.1 PFD CONTROLS 1 2 4 3 5 6 7 8 Figure 1-1 PFD Controls 9 13 10 14 11 15 12 1-2 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.
SECTION 1 SYSTEM OVERVIEW The following list provides an overview of the controls located on the PFD bezel (see Figure 1-1). 1 2 3 9 NAV VOL/ID Knob – Controls NAV audio volume level. Press to switch the Morse code identifier audio ON and OFF. Volume level is shown in the NAV frequency field as a percentage.
SECTION 1 SYSTEM OVERVIEW 1.2 CONTROLS ASSOCIATED WITH THE MFD The controls for the MFD (GDU 1500) are located on both the MFD bezel and the MFD Control Unit (GCU 475). The bottom portion of the MFD bezel features 12 softkeys that are designed to perform various functions depending upon the specific page being displayed. These softkeys are discussed throughout the Pilot’s Guide documentation.
SECTION 1 SYSTEM OVERVIEW 8 Plus (+) Minus (-) Key – Switches between a (+) or (-) character. 9 Decimal Key – Enters a decimal point. 10 SEL Key – The center of this key activates the selected softkey, while the right and left arrows move the softkey selection box to the right and left, respectively. 1 HDG Key – Selects/deselects Heading Select Mode. 2 APR Key – Selects/deselects Approach Mode. 3 NAV Key – Selects/deselects Navigation Mode.
SECTION 1 SYSTEM OVERVIEW 1-6 8 FLC Key – Selects/deselects Flight Level Change Mode. 9 CRS2 Knob – Sets the copilot-selected course on the HSI of PFD2 when the VOR1, VOR2, or OBS/SUSP mode is selected. Pressing this knob centers the CDI on the currently selected VOR. The copilot-selected course provides course reference to the copilot-side flight director when operating in Navigation and Approach modes. 10 SPD Key – Switches the Flight Level Change mode reference speed between IAS and MACH number.
SECTION 1 SYSTEM OVERVIEW 1.4 PFD SOFTKEY MAP Softkey ON Softkey OFF Figure 1-4 Top Level PFD Softkeys STRMSCP Select the BACK Softkey to return to the top-level softkeys.
SECTION 1 SYSTEM OVERVIEW Displays NEXRAD weather and coverage information on Inset Map (optional feature) Displays XM lightning information on Inset Map (optional feature) NEXRAD XM LTNG ADC1 ADC2 AHRS1 AHRS2 BACK MSG Select the BACK Softkey to return to the top level softkeys.
SECTION 1 SYSTEM OVERVIEW ALT UNIT HSI FRMT Select the BACK Softkey to return to the top-level softkeys 360 HSI ARC HSI METERS IN HPA Figure 1-7 PFD Configuration Softkeys Displays second-level softkeys for additional PFD configurations PFD DFLTS Resets PFD to default settings, including changing units to standard WIND Displays softkeys to select wind data parameters OPTN 1 Wind direction arrows with headwind and crosswind components OPTN 2 Wind direction arrow and speed OPTN 3 Wind directi
SECTION 1 SYSTEM OVERVIEW Displays softkeys for setting the altimeter and BARO settings to metric units ALT UNIT STD BARO METERS When enabled, displays altimeter in meters IN Select to display the BARO setting as inches of mercury HPA Select to display the BARO setting as hectopacals Sets barometric pressure to 29.92 in Hg (1013 hPa) MSG Select the BACK Softkey to return to the top-level softkeys. MSG Select the IDENT or BACK Softkey to return to the top-level softkeys.
SECTION 1 SYSTEM OVERVIEW 0—7 Use numbers to enter code BKSP Removes numbers entered, one at a time TMR/REF Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen Displays Timer/References Window NRST Displays Nearest Airports Window MSG Displays Messages Window IDENT 1.
SECTION 1 SYSTEM OVERVIEW Accesses the CAS scrolling softkeys. CAS CAS ↑ CAS ↓ Scroll up (Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling) Scroll down (Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling) Enables second-level Navigation Map softkeys TRAFFIC Displays traffic information on Navigation Map TOPO Displays topographical data (e.g.
SECTION 1 SYSTEM OVERVIEW Nearest Group Number of Pages in Current Group Auxiliary Page Group Waypoint Page Group Map Page Group Selected Page Figure 1-10 Page Group Icon 1.7 VERTICAL NAVIGATION One of two altitude sources is used by the G1000 when giving vertical navigation guidance. WAAS GPS altitude is used when giving guidance for a WAAS approach. Baro corrected altitude is used when vertical guidance is given in all other situations.
SECTION 1 SYSTEM OVERVIEW White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point. This altitude is provided as a reference and is not designated to be used in determining vertical speed and deviation guidance. Altitude has been entered by the pilot. Altitude is designated for use in giving vertical speed and deviation guidance.
SECTION 1 SYSTEM OVERVIEW Some altitudes retrieved from the database have associated restrictions indicating to stay ‘At’, ‘At or Above’, or ‘At or Below’ a specific altitude. These restrictions are indicated using a ‘bar’ above and/or below the appropriate altitude as shown in Figure 1-9. Cross AT or ABOVE 5,000 ft Cross AT 2,300 ft Cross AT or BELOW 3,000 ft Figure 1-12 Altitude Restrictions See Section 7 - Navigation, for a sample flight plan which further illustrates vertical navigation in more detail.
SECTION 1 SYSTEM OVERVIEW 3) Press the ENT Key to start the database update. A prompt similar to the following is displayed: database must be inserted into the bottom slot on the MFD. 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. When updating the terrain and FliteCharts databases, an ‘in progress’ message may be seen.
SECTION 1 SYSTEM OVERVIEW 1.10 PILOT PROFILES Figure 1-17 Pilot Profiles on AUX-System Setup Page Creating a Profile 8) Press the ENT Key. 1) Select the AUX - System Setup Page. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight ‘CREATE’ in the Pilot Profile Box. 4) Press the ENT Key. A ‘Create Profile’ window is displayed. 5) Use the FMS Knob to enter a profile name 6) Press the ENT Key.
SECTION 1 SYSTEM OVERVIEW Renaming a Profile 1) Select the AUX - System Setup Page. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight ‘RENAME’ in the Pilot Profile Box. 4) Press the ENT Key. 5) In the ‘Rename Profile’ window, turn the FMS Knob to select the profile to rename. 6) Press the ENT Key. 7) Use the FMS Knob to enter a new profile name up to 16 characters. 8) Press the ENT Key. 9) With ‘RENAME’ highlighted, press the ENT Key.
SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated.
SECTION 2 FLIGHT INSTRUMENTS 1 2 16 15 3 4 14 5 13 6 12 7 11 8 9 10 1 AFCS Status Annunciation 9 DME Information Window 2 Traffic Annunciation 10 BRG2 Information Window 3 Vspeed References 11 Flight Plan Window 4 Radar Altimeter Indication 12 Barometric/Radar Altimeter Minimums Window 5 Selected Heading Window 13 Selected Course Window 6 Wind Data Window 14 Altitude Reference Bug 7 Inset Map 15 Barometric/Radar Altimeter Minimums Bug 8 BRG1 Information Window 16 V
SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Speed Ranges Airspeed Trend Vector The end of the trend vector displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration/deceleration is maintained. Vspeed References Airspeed Trend Vector Actual Airspeed Vspeed References Vspeeds are set using the TMR/REF Softkey. When active (ON), the Vspeeds are displayed at their respective locations to the right of the airspeed scale.
SECTION 2 FLIGHT INSTRUMENTS 2.3 ALTIMETER Barometric Setting Box Altitude Reference Box Select barometric pressure: Turn the BARO Knob to select the desired setting. Quickly enter standard pressure: 1) Select the PFD Softkey. Altitude Trend Vector Current Altitude Barometric/Radar Altimeter Altitude Minimums Bug 2) Select the STD BARO Softkey. Synchronizing Altimeter Baro Settings 1) Select the AUX - System Setup Page using the FMS Knob.
SECTION 2 FLIGHT INSTRUMENTS 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight ‘Altitude’ in the ‘Baro Transition Alert’ box. 4) Turn the small FMS Knob to turn the alert OFF or ON and press the ENT Key. 5) Turn the small FMS Knob to change the altitude and press the ENT Key. 6) To cancel the selection, press the FMS Knob. Metric Display Display altitude in meters and barometric pressure in hectopascals: 1) Select the PFD Softkey to display the second level softkeys.
SECTION 2 FLIGHT INSTRUMENTS VNV Target Altitude Low Altitude Annunciation Vertical Deviation Indicator Required Vertical Speed Figure 2-10 Low Altitude on GPS Approach 2.4 VERTICAL DEVIATION/GLIDEPATH/ GLIDESLOPE INDICATOR Figure 2-11 Vertical Deviation Indications NOTE: VNV altitudes displayed on the Active Flightplan Page must be designated for use in vertical guidance.
SECTION 2 FLIGHT INSTRUMENTS 2.6 Marker Beacon Annunciation VERTICAL SPEED INDICATOR Glideslope Indicator Vertical Speed Pointer Figure 2-15 Vertical Speed Indicator Figure 2-13 Glideslope Indicator 2.5 MARKER BEACON ANNUNCIATIONS The actual vertical speed is displayed inside the pointer. 2.7 Outer Marker Middle Marker Inner Marker BAROMETRIC/RADAR ALTITUDE MINIMUMS The desired barometric/radar altitude minimums can be set in the Timer/References Window.
SECTION 2 FLIGHT INSTRUMENTS The desired barometric/radar minimum descent altitude (MDA, or Decision Height, DH) can be set in the Timer/References Window. Visual annunciations alert the pilot when approaching the MDA: • When the aircraft altitude descends to within 2500 feet of the MDA setting, the BARO MIN or RA MIN Box (depending on the selected source) appears with the altitude in light blue text. The bug appears on the tape in light blue once in range.
SECTION 2 FLIGHT INSTRUMENTS 2.9 WIND DATA When the window is selected for display, but wind information is invalid or unavailable, the window shows “NO WIND DATA”. Wind data can be displayed in three different ways: • Wind direction arrows with headwind and crosswind components (Option 1) • Wind direction arrow and speed (Option 2) • Wind direction arrow with direction and speed (Option 3) Option 1 Option 2 2.
SECTION 2 FLIGHT INSTRUMENTS Turn Rate Indicator and Heading Trend Vector Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta turn rate trend vector shows the current turn rate. The end of the trend vector gives the heading predicted in six seconds, based on the present turn rate. At rates greater than 4 deg/sec, an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid.
Departure Enroute Terminal (Oceanic if >200 nm from nearest airport) Terminal Refer to accompanying approach CDI scaling figures Approach 0.3 nm 1.0 nm 1.0 nm 2.0 nm 1.0 nm 0.3 nm CDI Full-scale Deflection SECTION 2 FLIGHT INSTRUMENTS Missed Approach Drawing not to scale 0.3 nm angle set by system 350 ft CDI scale is set to the smaller of 0.3 nm or an angle set by the system 1.
SECTION 2 FLIGHT INSTRUMENTS Bearing Pointers and Information Windows DME (optional) Selecting the PFD Softkey provides access to the BRG1 and BRG2 Softkeys. The BRG1 Pointer is a single line pointer. The BRG2 Pointer is a double line pointer. To display the DME Information Window, select the PFD Softkey followed by the DME Softkey.
SECTION 2 FLIGHT INSTRUMENTS 2.11 GENERIC TIMER Figure 2-32 Timer Status Prompts Change the Generic Timer: 1) Select the TMR/REF Softkey, then turn the large FMS Knob to select the time field (hh/mm/ss). Turn the FMS Knobs to set the desired time, then press the ENT Key. The UP/DOWN field is now highlighted. Figure 2-31 GPS LOI, GPS SUSP, LOC1 and VOR2 Enable/disable OBS Mode while navigating with GPS: 1) Select the OBS Softkey to select OBS Mode.
SECTION 2 FLIGHT INSTRUMENTS Blank Page 2-14 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.
SECTION 3 – ENGINE & AIRFRAME SYSTEMS SECTION 3: ENGINE & AIRFRAME SYSTEMS 1 1 8 2 2 9 10 3 11 3 4 4 12 13 5 14 5 6 6 15 7 16 17 8 9 17 12 13 15 16 Figure 3-2 EIS Display (Reversionary Mode) Figure 3-1 EIS Display (Normal Mode) 1 Torque 7 CAS Display 2 Propeller Speed 8 Cabin Pressure Altitude and Change Rate 14 Fuel Pressure 3 Generator Speed 9 Differential Pressure 15 Battery and Generator Currents 4 Interturbine Temperature 10 Selected Cabin Altitude 16 Bat
SECTION 3 – ENGINE & AIRFRAME SYSTEMS Green ranges on the instrument scales indicate normal ranges of operation; yellow and red bands indicate caution and warning, respectively. During normal operating conditions, an instrument’s pointer appears in white and the readout text is green. When data is out of the range of the indicator or gauge, the pointer moves to the end of the scale; readouts display as “___”. Temperatures above which warnings occur are indicated by red tick marks along the ITT Gauge. 3.
SECTION 3 – ENGINE & AIRFRAME SYSTEMS Active generator currents are displayed below the generator icons. A disconnected generator is indicated in gray; the current is removed from the display and the switch symbol is closed. Switch Open Switch Closed Main Battery and essential bus voltages are displayed using gauges. Power buses are shown in green when energized. When not energized, the connection line to the main bus is removed and the bus label is displayed in red.
SECTION 3 – ENGINE & AIRFRAME SYSTEMS 3.2 FUEL SYSTEM Pressing the SYSTEM Softkey displays the softkeys for the synoptics system. Press the FUEL Softkey to display the Fuel System Page. The Fuel Synoptics Page displays the status of the fuel tanks and feed system. Fuel quantity is depicted graphically; the color changes to yellow if the fuel quantity drops below the threshold level.
SECTION 3 – ENGINE & AIRFRAME SYSTEMS Status of the fuel selector is indicated between the fuel tank symbols. The mode, automatic (AUTO), manual (MAN), or off (no indication; CAS message ‘FUEL OFF’ generated) is shown beneath the fuel selector symbol. Left Fuel Tank Selected Switching Fuel Tank Selection Right Fuel Tank Selected Unknown Fuel Tank Selection Table 3-2 Fuel Selector Status If the auxiliary fuel boost pump is on, the symbol is displayed in green.
SECTION 3 – ENGINE & AIRFRAME SYSTEMS 3.3 GENERAL SYSTEMS Pressing the SYSTEM Softkey displays the softkeys for the synoptics system. Press the GEN Softkey to display the General System Page. The General Synoptics Page aircraft diagram displays open doors in red (CAS messages also generated).
SECTION 3 – ENGINE & AIRFRAME SYSTEMS 3.4 CREW ALERTING SYSTEM (CAS) NOTE: Refer to the Pilot’s Operating Handbook (POH) for emergency procedures. Up to 14 messages can be displayed; when more than 14 messages accumulate, the scrolling CAS softkeys become available.
SECTION 3 – ENGINE & AIRFRAME SYSTEMS Messages Comments BAT OVERHEAT BLEED TEMP CABIN ALTITUDE CABIN DIFF PRESS DOOR FIRE FLAPS ASYM FUEL OFF FUEL PRESS ITT OIL PRESS OXYGEN PARK BRAKE TORQUE ENGINE OFF ENGINE ON GROUND TOPI AIR LOPI Inhibits Battery temperature over 70°C Bleed temperature high X Cabin altitude over 10,000 ft Cabin pressure differential over 6.
Messages Comments AUTO SEL AUX BOOST PMP ON BAT AMP BAT OFF BLEED OFF CHIP FRONT CARGO DOOR Fuel timer off or out of service Electric fuel pump running (manual or automatic mode) Battery current over 50 A while on ground Battery off Flow control and shut-off valve/shut-off valve closed Oil chip detector on (if installed) Forward baggage door open Fuel tanks imbalanced by more than 15 USGAL for > 30 seconds Fuel quantity less than or equal to 9.
SECTION 3 – ENGINE & AIRFRAME SYSTEMS Display Inhibits Inhibits prevent certain CAS messages from being displayed during the following conditions: • Engine off • Engine on • Aircraft on ground • Takeoff • Aircraft in air • Landing Takeoff and Landing Operation Phase inhibits (TOPI and LOPI) are implemented to reduce flight crew workload and distractions during takeoff and landing. Alerts affected by an inhibit are not displayed while the inhibit is enabled.
SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER The NAV/COM controls and frequency boxes share the same locations on both Primary Flight Displays. NAV Controls NAV Frequency Box COM Frequency Box COM Controls Figure 4-1 G1000 VHF NAV/COM Controls (PFD shown) 190-00708-00 Rev.
SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Tuning Box Selected NAV Frequency Selected COM Frequency Figure 4-2 Frequency Fields Active NAV Frequency Field Frequency Transfer Arrow Active COM Frequency Field Standby COM Frequency Field Tuning Box Tuning Box Figure 4-3 Frequency Transfer Arrow and Tuning Box NAV Controls COM Controls VOL/PUSH ID Knob VOL/PUSH SQ Knob Frequency Transfer Key Dual NAV Knob Dual COM Knob • Turn to tune in desired frequencies.
SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS 4.4 QUICKLY ACTIVATING 121.500 MHZ • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception. Pressing and holding the COM Frequency Transfer Key for approximately two (2) seconds automatically tunes the selected COM radio to the emergency frequency. • TX – When a COM radio is transmitting, a white ‘TX’ indication appears to the right of the corresponding COM frequency. 4.
SECTION 4 – NAV/COM & TRANSPONDER DME Radio (optional) The DME Tuning Window is displayed by selecting the DME Softkey. 1) Select the NRST Softkey to display the Nearest Airports Window. 2) Turn either FMS Knob to highlight the desired frequency. 3) Press the ENT Key to place the frequency in the standby field of the active COM. 4) Press the Frequency Transfer Key to place the frequency in the active field.
SECTION 4 – NAV/COM & TRANSPONDER Reply Status Figure 4-11 Ground Mode Standby Mode (Manual) When the transponder sends replies to interrogations, an “R” indication appears momentarily in the reply status field. Reply Indication Select the STBY Softkey. In Standby Mode, the transponder does not reply to interrogations, but new codes can be entered.
SECTION 4 – NAV/COM & TRANSPONDER Enter Code Using the FMS Knob 1) Select the XPDR Softkey to display the transponder Mode Selection softkeys. 2) Select the CODE Softkey to display the transponder Code Selection softkeys, which includes the digit softkeys. 3) Turn the small FMS Knob to enter the first two digits. 4) Turn the large FMS Knob to place the cursor in position to change the second two digits. 5) Turn the small FMS Knob to enter the second two digits.
SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transmitters (COM3 MIC is unavailable) Transceiver Audio (COM 3 is unavailable) Passenger Address Telephone (Unavailable) Music Speaker Marker Beacon/Mute Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio Aircraft Navigation Radio Audio (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 Fig
SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Outer Marker Middle Marker Inner Marker Pressing the COM1 MIC or COM2 MIC Key selects the active transmitter (i.e., microphone). The associated receiver audio (COM1 or COM2) also becomes selected when the COM MIC Key is pressed. Altimeter Figure 5-4 Marker Beacon Annunciators on the PFD Figure 5-2 Transceivers 5.2 MUSIC SELECTION Pressing the MUSIC Key turns music on or off.
SECTION 5 – AUDIO PANEL 5.5 PASSENGER ADDRESS SYSTEM A passenger address system is activated by pressing the PA Key to deliver messages to the passengers. The message is heard by the other pilot on the headset only if the INTR COM Key is enabled. PA messages are one way from the flight deck to the passengers. A Push-to-talk (PTT) must be pressed to deliver PA announcements to the passengers over their headphones.
SECTION 5 – AUDIO PANEL • Pressing PLAY once plays the latest recorded memory block, then returns to normal operation. • Pressing MKR/MUTE while playing a memory block stops play. • Pressing the PLAY Key during play begins playing the previously recorded memory block. Each subsequent press of the PLAY Key begins playing the next previously recorded block. If a COM input signal is detected while playing, play is halted and the new COM input signal is recorded as the latest block.
SECTION 6 – AUTOMATIC FLIGHT CONTROL SECTION 6: AUTOMATIC FLIGHT CONTROL 6.1 FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in Table 6-1 (when the flight director is not active) activates the pilot-side flight director in the listed modes. The flight director may be turned off and the Command Bars removed from the displays by pressing the FD Key again. The FD Key is disabled when the autopilot is engaged.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Lateral Modes Armed Active Autopilot Status Yaw Damper Status Flight Director Indicator Arrow Active Vertical Modes Mode Reference Armed AFCS Status Box Selected Altitude Vertical Speed Reference Command Bars GPS is Selected Navigation Source Figure 6-1 PFD AFCS Display 6.2 SWITCHING FLIGHT DIRECTORS Only one flight director is active (selected) at a time. Flight directors may be switched by pressing the XFR Key on the AFCS Control Unit.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.3 COMMAND BARS Upon activation of the flight director, Command Bars are displayed in magenta on the PFDs as single cues or cross pointers. The Aircraft Symbol (in yellow) changes to accommodate the Command Bar format; the Command Bars do not override the Aircraft Symbol. The single-cue Command Bars (Figure 6-3) move together vertically to indicate pitch commands and bank left or right to indicate roll commands.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.4 FLIGHT DIRECTOR MODES Unless otherwise specified, all mode keys are alternate action (i.e., press on, press off). In the absence of specific mode selection, the flight director reverts to the default pitch and/or roll modes(s). Armed modes are annunciated in white and active modes in green in the AFCS Status Box. Under normal operation, when the control for the active flight director mode is pressed, the flight director reverts to the default mode(s) for the axis(es).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Mode Pitch Hold Selected Altitude Capture Altitude Hold Vertical Speed Description Control Annunciation Holds the current aircraft pitch attitude; may be used to climb/descend to the (default) Selected Altitude PIT Captures the Selected Altitude ALTS * Holds the current Altitude Reference ALT Key Maintains the current aircraft vertical speed; may be used to climb/descend VS Key to the Selected Altitude Flight Level Change, Maintains the current aircraf
SECTION 6 – AUTOMATIC FLIGHT CONTROL Pitch Hold Mode (PIT) Changing the Pitch Reference When the flight director is activated (the FD Key is pressed) or switched, Pitch Hold Mode is selected by default. Pitch Hold Mode is indicated as the active vertical mode by the ‘PIT’ annunciation. This mode may be used for climb or descent to the Selected Altitude (shown above the Altimeter), since Selected Altitude Capture Mode is automatically armed when the mode is activated.
SECTION 6 – AUTOMATIC FLIGHT CONTROL The white ‘ALTS’ annunciation indicates Selected Altitude Capture Mode is armed (see Figure 6-7). The ALT SEL Knob is used to set the Selected Altitude (shown above the Altimeter) until Selected Altitude Capture Mode becomes active. As the aircraft nears the Selected Altitude, the flight director automatically transitions to Selected Altitude Capture Mode with Altitude Hold Mode armed (Figure 6-8).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Speed Mode (VS) Changing the Vertical Speed Reference In Vertical Speed Mode, the flight director acquires and maintains a Vertical Speed Reference. Current aircraft vertical speed (to the nearest 100 fpm) becomes the Vertical Speed Reference at the moment of Vertical Speed Mode activation.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flight Level Change Mode (FLC) NOTE: The Selected Altitude should be set before selecting Flight Level Change Mode. Flight Level Change Mode is selected by pressing the FLC Key. This mode acquires and maintains the Airspeed Reference while climbing or descending to the Selected Altitude (shown above the Altimeter). When Flight Level Change Mode is active, the flight director continuously monitors Selected Altitude, airspeed, Mach, and altitude.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Changing the Airspeed Reference The Airspeed Reference (shown in both the AFCS Status Box and above the Airspeed Indicator) may be adjusted by: • Using the NOSE UP/DN Wheel • Pressing the CWS Button, hand-flying the aircraft to attain a new Airspeed Reference, then releasing the CWS Button Vertical Navigation Modes (VPTH, ALTV) NOTE: VNV is disabled when parallel track or Dead Reckoning Mode is active.
SECTION 6 – AUTOMATIC FLIGHT CONTROL • Pressing the VNV Key • Adjusting the Selected Altitude If acknowledgment is not received within 1 minute of descent path interception, the white ‘VPTH’ annunciation and the VNV Key annunciator light start to flash. Flashing continues until acknowledged or the descent path is intercepted. If the descent is not confirmed by the time of interception, Vertical Path Tracking Mode remains armed and the descent is not captured.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Path Tracking Active VNV Target Altitude Capture Armed VNV Target Altitude Vertical Deviation Indicator (VDI) Required Vertical Speed Indication (RSVI) GPS is Selected Navigation Source Terminal Phase of Flight Figure 6-13 Vertical Path Tracking Mode Automatic Reversion to Pitch Hold Mode Several situations can occur while Vertical Path Tracking Mode is active which cause the flight director to revert to Pitch Hold Mode: • Vertical deviation exceeds 200 fe
SECTION 6 – AUTOMATIC FLIGHT CONTROL To prevent immediate profile re-capture, the following must be satisfied: • At least 10 seconds have passed since the non-path transition was initiated • Vertical deviation from the profile has exceeded 250 feet, but is now less than 200 feet Pressing the VNV Key twice re-arms Vertical Path Tracking for immediate profile re-capture. VNV Target Altitude Capture Mode (ALTV) NOTE: Armed VNV Target Altitude and Selected Altitude capture modes are mutually exclusive.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Glidepath Mode (GP) NOTE: Pressing the CWS Button while Glidepath Mode is active does not cancel the mode. The autopilot guides the aircraft back to the glidepath upon release of the CWS Button. Glidepath Mode is used to track the WAAS-based glidepath. When Glidepath Mode is armed, ‘GP’ is annunciated in white in the AFCS Status Box. Selecting Glidepath Mode 1) Ensure a GPS approach is loaded into the active flight plan.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Glideslope Mode (GS) NOTE: Pressing the CWS Button while Glideslope Mode is active does not cancel the mode. The autopilot guides the aircraft back to the glideslope upon release of the CWS Button. Glideslope Mode is available for LOC/ILS approaches to capture and track the glideslope. When Glideslope Mode is armed (annunciated as ‘GS’ in white), LOC Approach Mode is armed as the lateral flight director mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Takeoff (TO) and Go Around (GA) Modes Go Around and Takeoff modes are coupled pitch and roll modes and are annunciated as both the vertical and lateral modes when active. In these modes, the flight director commands a constant set pitch attitude and keeps the wings level. The GA Switch is used to select both modes. The mode entered by the flight director depends on whether the aircraft is on the ground.
SECTION 6 – AUTOMATIC FLIGHT CONTROL • Low Bank — Limits the maximum commanded roll angle • Heading Select — Captures and tracks the Selected Heading • Navigation — Captures and tracks the selected navigation source (GPS, VOR, LOC) • Backcourse — Captures and tracks a localizer signal for backcourse approaches • Approach — Captures and tracks the selected navigation source (GPS, VOR, LOC) Lateral Mode • Takeoff — Commands a constant pitch angle and wings level on the ground in preparation for takeoff • Go
SECTION 6 – AUTOMATIC FLIGHT CONTROL Roll Hold Mode (ROL) Low Bank Mode NOTE: If Roll Hold Mode is activated as a result of a mode reversion, the flight director rolls the wings level. When the flight director is activated or switched, Roll Hold Mode is selected by default. This mode is annunciated as ‘ROL’ in the AFCS Status Box as shown in Figure 6-21. The current aircraft bank angle is held, subject to the bank angle conditions in Table 6-4.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Heading Select Mode (HDG) Heading Select Mode is activated by pressing the HDG Key. Heading Select Mode acquires and maintains the Selected Heading. The Selected Heading is shown by a light blue bug on the HSI and in the box to the upper left of the HSI. Turns are commanded in the same direction as Selected Heading Bug movement, even if the bug is turned more than 180° from the present heading (e.g., a 270° turn to the right).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Navigation Mode (GPS, VOR, LOC) NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the flight director to enter Navigation Mode. Pressing the NAV Key selects Navigation Mode. Navigation Mode acquires and tracks the selected navigation source (GPS, VOR, LOC). The flight director follows GPS roll steering commands when GPS is the selected navigation source.
SECTION 6 – AUTOMATIC FLIGHT CONTROL If Navigation Mode is active and either of the following occur, the flight director reverts to Roll Hold Mode (wings rolled level): • Different VOR tuned while in VOR Navigation Mode (VOR Navigation Mode reverts to armed) • Navigation source manually switched (with the CDI Softkey) • FAF crossed while in GPS Navigation Mode after the automatic navigation source switch from GPS to LOC Selecting VOR Approach Mode 1) Ensure a valid VOR frequency is tuned 2) Ensure that V
SECTION 6 – AUTOMATIC FLIGHT CONTROL Selecting LOC Approach Mode 1) Ensure a valid localizer frequency is tuned. 2) Ensure that LOC is the selected navigation source (use the CDI Softkey to cycle through navigation sources if necessary). 3) Press the APR Key. Changing the Selected Course The Selected Course on each PFD is controlled using the CRS1 and CRS2 knobs. Pressing the CWS Button and hand-flying the aircraft does not change the Selected Course while in Approach Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Backcourse Mode (BC) Changing the Selected Course NOTE: When making a backcourse approach, set the Selected Course to the localizer front course. Backcourse Mode captures and tracks a localizer signal in the backcourse direction. The mode may be selected by pressing the BC Key. Backcourse Mode is armed if the CDI is greater than one dot when the mode is selected.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.5 AUTOPILOT AND YAW DAMPER OPERATION are generated only when both halves of the MEPT Switch are operated simultaneously. Trim speeds are scheduled with airspeed to provide more consistent response. NOTE: Refer to the AFM for specific instructions regarding emergency procedures. Roll Axis The autopilot roll axis uses roll rate to stabilize aircraft roll attitude during upsets and flight director maneuvers.
SECTION 6 – AUTOMATIC FLIGHT CONTROL When the YD Key is pressed, the system engages the yaw damper independently 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’ annunciations, respectively. Control Wheel Steering During autopilot operation, the aircraft may be handflown without disengaging the autopilot.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.6 PROCEDURES Departure Climbing to the Selected Altitude and flying an assigned heading: NOTE: The diagrams in this section are for instructional purposes only and should not be used for navigation. Numbered portions of accompanying diagrams correspond to numbered procedure steps. 1) Depart KMKC: a) Use the ALT SEL Knob to set the Selected Altitude to 12,000 feet before takeoff.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 2) In this example, Vertical Speed Mode is used to capture the Selected Altitude (Pitch Hold, Vertical Speed, or Flight Level Change Mode may be used). 3) Use the HDG Knob to set the Selected Heading, complying with ATC vectors to intercept Airway V4. a) Adjust the aircraft’s vertical speed to the desired 500 fpm. Press the HDG Key to activate Heading Select Mode while the autopilot is engaged in the climb.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial d) Press the NAV Key. This arms VOR Navigation Mode and the white ‘VOR’ annunciation appears to the left of the active lateral mode. During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Airway V4 to Salina VOR (SLN) should now be intercepted. Since the enroute flight plan waypoints correspond to VORs, flight director Navigation Mode using either VOR or GPS as the navigation source may be used.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a Flight Plan/GPS Course 2) Following the flight plan, the autopilot continues to steer the aircraft under GPS guidance. Note that in GPS Navigation Mode, course changes defined by the flight plan are automatically made without pilot action required. NOTE: Changing the navigation source cancels Navigation Mode and causes the flight director to revert back to Roll Hold Mode (wings rolled level).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Descent While flying the arrival procedure, the aircraft is cleared for descent in preparation for the approach to KCOS. Three methods are presented for the descent from 12,000 ft: • Flight Level Change descent – Flight Level Change Mode can be used to descend to the Selected Altitude at a constant airspeed. This descent method does not account for flight plan waypoint altitude constraints.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Path Tracking descent to VNV Target Altitude: • Turn the ALT Knob to adjust the Selected Altitude • Press the VNV Key 1) Select VNV flight control: a) Press the VNV Key to arm Vertical Path Tracking Mode. The white annunciation ‘VPTH’ appears. b) Using the ALT Knob, set the Selected Altitude at least 75 feet below the flight plan’s VNV Target Altitude of 10,000 feet.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Non-path descent using Flight Level Change Mode: 1) Command a non-path descent using Flight Level Change Mode: The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude; the autopilot transitions to Altitude Hold Mode and levels the aircraft. a) Using the ALT Knob, set the Selected Altitude below the current aircraft altitude to an altitude (in this case, 9,400 feet) at which to level off between VNV flight plan altitudes.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Approach KCOS 1) Transition from GPS Navigation Mode to Heading Select Mode. 3 a) Select the Runway 35L ILS approach for KCOS into the flight plan and select ‘VECTORS’ for the transition. PETEY G e od M PYNON 1 GPS NAV Mode c) Press the HDG Key. The autopilot turns the aircraft to the desired heading. 2 HD b) Use the HDG Knob to set the Selected Heading after getting vectors from ATC.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a WAAS precision approach: KCOS 1) Arm flight director modes for a precision approach: 4 a) Make sure the navigation source is set to GPS (use CDI Softkey to change navigation source). 2) Press the APR Key once clearance for approach has been acquired. GPS Approach Mode is activated and Glidepath Mode is armed. CEGIX 3 GPS APR/ GP Mode b) Select the Runway 35R LPV approach for KCOS into the flight plan.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go Around/Missed Approach Flying a missed approach: 1) Push the GA Switch at the Decision height and apply full power to execute a missed approach. The flight director Command Bars establish a nose-up climb to follow. Note that when the GA Switch is pushed, the missed approach is activated and the autopilot disconnects, indicated by the ‘AP’ annunciation flashing yellow for 5 seconds.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.7 AFCS ANNUNCIATIONS AND ALERTS AFCS Status Annunciation AFCS Status Alerts The annunciations in Table 6-4 (listed in order of increasing priority) can appear on the PFDs above the Airspeed and Attitude indicators. Only one annunciation may occur at a time, and messages are prioritized by criticality.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Overspeed Protection While Pitch Hold, Vertical Speed, Flight Level Change, Vertical Path Tracking, or an altitude capture mode is active, airspeed is monitored by the flight director and pitch commands are limited for overspeed protection. Overspeed protection is provided in situations where the flight director cannot acquire and maintain the mode reference for the selected vertical mode without exceeding the certified maximum autopilot airspeed.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Blank Page 6-38 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.
SECTION 7 – NAVIGATION SECTION 7: NAVIGATION The majority of the following discussions pertain to the Multi Function Display. In discussions pertaining to the PFD, the controls are located on the PFD. 7.1 NAVIGATION MAP PAGE WARNING: The map display should only be used for situational awareness. Any map display indication should be compared with approved navigation sources.
SECTION 7 – NAVIGATION 9) Press the ENT Key. The cursor is placed in the ‘VNV’ offset distance field. 10) Enter the desired target altitude offset from the selected Direct-to. 11) Press the ENT Key to highlight ‘Activate?’ or turn the large FMS Knob to highlight the ‘COURSE’ field. Select a Direct-to Destination to a Nearest Airport 1) Press the Direct-to ( ) Key. 2) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed as in Figure 7-3.
SECTION 7 – NAVIGATION 10) Enter the desired course. 11) Press the ENT Key. The cursor now highlights ‘ACTIVATE?’. 12) Press the ENT Key again to begin navigation using the selected destination, altitude constraint, and course. Figure 7-5 Recently Entered Waypoints List (MFD) 3) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints as shown in Figure 7-5. 4) Turn the large FMS Knob to select the desired airport. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’.
SECTION 7 – NAVIGATION Enter a Direct-to Destination 1) Press the Direct-to Key ( ). Select a Direct-to Destination to a Flight Plan Waypoint 2) Turn the large FMS Knob to place the cursor in the desired selection field. 1) While navigating an active flight plan, press the Direct-to ( ) Key. 3) Turn the small FMS Knob to begin selecting the desired identifier, location, etc. 2) Turn the small FMS Knob to the left to display a list of flight plan waypoints as shown in Figure 7-8. 4) Press the ENT Key.
SECTION 7 – NAVIGATION 4) Turn the large FMS Knob to select the desired airport. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 6) Press ENT again to activate a Direct-to. Select a Direct-to Destination to a Recently Entered Identifier 1) Press the Direct-to ( ) Key. 2) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed as in Figure 7-8. The list is only populated when navigating a flight plan.
SECTION 7 – NAVIGATION 2) Figure 7-11 shows the aircraft on the assigned heading of 240º. ‘TERM’ (Terminal) is the current CDI flight phase displayed on the HSI indicating 1.0 nm CDI scaling. 3) ATC now assigns routing to join V4. A heading of 290º is assigned to intercept V4. The aircraft turns to heading 290° as seen in Figure 7-12. Figure 7-12 Assigned Heading of 290º Figure 7-11 Assigned Heading of 240º 7-6 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.
SECTION 7 – NAVIGATION 4) V4 is now be entered into the flight plan. a) Press the FMS Knob to activate the cursor. b) The desired entry point for V4 (TOP) must now be entered. Turn the large FMS Knob to highlight the desired flight plan insertion point as shown in Figure 7-13. The V4 entry point (TOP) will be placed immediately above the highlighted waypoint (SLN). c) Turn the small FMS Knob to display the Waypoint Information Window.
SECTION 7 – NAVIGATION e) With SLN still highlighted as in Figure 7-15, turn the small FMS Knob to the right. The Waypoint Information Page is displayed and the LD AIRWY Softkey is now available. f) Select the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 7-16. Figure 7-17 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 seen in Figure 7-17.
SECTION 7 – NAVIGATION l) V4 is now loaded into the flight plan as shown in Figure 7-19. on the HSI indicating 16.9 nm to the intercept point. Note the phase of flight remained in Terminal (TERM) mode up to this point because a departure leg was active. Since a leg after the departure is now active, the current CDI flight phase is ENR (Enroute) and CDI scaling has changed to 2.0 nm. Figure 7-19 V4 is Loaded in the Flight Plan 5) V4 is now made the active leg of the flight plan.
SECTION 7 – NAVIGATION on the last dot indicating a 2.0 nm distance from the centerline of the next course. 7) As the CDI approaches center, the aircraft turns onto the active leg as seen in Figure 7-22. 8) At SLN, Victor Airway 244 (V244) is intercepted. Turn prompts are displayed in the PFD Navigation Status Box as seen in Figure 7-23. Figure 7-23 Turn to Intercept V244 9) As seen in Figure 7-24, V244 is now the active flight plan leg.
SECTION 7 – NAVIGATION 10) At Lamar VOR (LAA) V263 is intercepted. See Figure 7-25. Figure 7-26 Direct To OPSHN d) Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 7-27. Figure 7-25 HYS to LAA Leg Active 11) ATC grants clearance to proceed direct to 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 cursor.
SECTION 7 – NAVIGATION f) Press the ENT Key. The cursor is now displayed in the VNV offset field as shown in Figure 7-28. NOTE: If the loaded arrival procedure has waypoints with altitude constraints retrieved from the database that will be used as is, the altitude must be manually accepted by placing the cursor over the desired altitude, then pressing the ENT Key. The altitude is now displayed as light blue meaning it is now being used by the system to determine vertical speed and deviation guidance.
SECTION 7 – NAVIGATION b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 7-30. d) Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 7-31. e) Press the ENT Key. A list of available transitions for the selected approach is displayed as shown on Figure 7-32. Figure 7-30 Procedures Window c) Press the ENT Key. A list of available approaches for the destination airport is displayed as in Figure 7-31.
SECTION 7 – NAVIGATION h) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen in Figure 7-33. b) Turn the large FMS Knob to place the cursor in the altitude field associated with the IAF at HABUK as in Figure 7-34. Figure 7-34 Designate HABUK Altitude Constraint Figure 7-33 Loaded Approach 13) Note the altitude constraints associated with each of the approach waypoints as seen in Figure 7-33.
SECTION 7 – NAVIGATION d) Turn the large FMS Knob to select the altitude constraint associated with FALUR as seen in Figure 7-35. Altitude constraint values associated with the Final Approach Fix (FAF) and waypoints beyond the FAF cannot be designated for vertical guidance. These altitude values are always displayed as white text, as in Figure 7-36.
SECTION 7 – NAVIGATION a) Select the VNV PROF Softkey to place the cursor in the target vertical speed field (VS TGT) as shown in Figure 7-37. 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 field, then turn the small FMS Knob to enter the desired value. 15) As seen in Figure 7-38, the aircraft is approaching TOD. Note the target vertical speed required to reached the selected altitude.
SECTION 7 – NAVIGATION 16) Upon reaching TOD, a descent vertical speed is established which places the VSI pointer in line with the RVSI as shown in Figure 7-40. Keep Vertical Deviation Pointer Centered 18) The aircraft is approaching OPSHN. The upcoming turn and next heading is annunciated at the top left of the PFD as seen in Figure 7-42. Initiate the turn and maneuver the aircraft on a track through the turn radius to intercept the magenta line for the OPSHN to FSHER leg and center the CDI.
SECTION 7 – NAVIGATION 19) After passing OPSHN, the next leg of the arrival turns magenta as shown in Figure 7-43. The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active. Figure 7-43 Tracking the OPSHN to FSHER Leg 20) The flight continues through the arrival procedure to PYNON (see Figure 7-44).
SECTION 7 – NAVIGATION 21) Upon passing PYNON the approach procedure automatically becomes active. The approach may be activated at any point to proceed directly to the IAF. In this example, the aircraft has progressed through the final waypoint of the arrival and the flight plan has automatically sequenced to the IAF as the active leg, activating the approach procedure (see Figure 7-45). c) Press the ENT Key to activate the approach. 22) The IAF is the next waypoint.
SECTION 7 – NAVIGATION 23) After crossing FALUR the next waypoint is the FAF. The flight phase changes to LPV on the HSI indicating the current phase of flight is in Approach Mode and the approach type is LPV. CDI scaling changes accordingly and is used much like a localizer when flying an ILS approach. The RVSI is no longer displayed and the VDI changes to the Glidepath Indicator (as shown in Figure 7-48) when the final approach course becomes active.
SECTION 7 – NAVIGATION In this missed approach procedure, the fix immediately following the MAP (in this case ‘6368FT’) is not part of the published procedure. It is simply a fix that defines a leg which guides the aircraft along the runway centerline until the required altitude to make the first turn on the missed approach is exceeded.
SECTION 7 – NAVIGATION 26) The aircraft continues climbing to “AT or ABOVE” 10,000 feet at MOGAL. A holding pattern is established at the MAHP (MOGAL) as shown in Figure 7-51. 27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 752. Figure 7-52 Hold Established Figure 7-51 Establishing the Holding Pattern 7-22 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.
SECTION 7 – NAVIGATION 7.4 AIRPORT INFORMATION Select an Airport from the Active Flight Plan 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the small FMS Knob to the left to display a list of flight plan airports as shown in Figure 7-54. Figure 7-54 Flight Plan Airport List 3) Turn the large FMS Knob to select the desired airport. 4) Press the ENT Key.
SECTION 7 – NAVIGATION 4) Turn the large FMS Knob to select the desired airport. 5) Press the ENT Key. Select a Recently Entered Airport Identifier 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the small FMS Knob to the left. Initially, a flight plan waypoint list is displayed as in Figure 7-54. The list is populated only when navigating a flight plan. 3) Turn the small FMS Knob to the right to display the ‘RECENT’ airports as shown in Figure 7-56.
SECTION 7 – NAVIGATION 7.5 INTERSECTION INFORMATION 7.6 NDB INFORMATION Select the Intersection Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the second rectangular page icon. Figure 7-58 NDB Information Page Select the NDB Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group.
SECTION 7 – NAVIGATION 7.7 VOR INFORMATION 7.8 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user defined waypoints. 7.9 NEAREST AIRPORTS Figure 7-59 VOR Information Page Select the VOR Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the fourth rectangular page icon.
SECTION 7 – NAVIGATION Access Information on a Specific Airport 1) With the Nearest Airports Page displayed, select the APT Softkey to place the cursor in the ‘NEAREST AIRPORTS’ field. The first airport in the nearest airports list is highlighted. Nearest Airports Information on the PFD Bearing TO Distance Airport Symbol Identifier Runway Length 2) Press the FMS Knob, then turn the large FMS Knob to highlight the desired airport. 3) Press the FMS Knob to remove the flashing cursor.
SECTION 7 – NAVIGATION 7.10 NEAREST INTERSECTIONS Figure 7-62 Nearest Intersections Page Select the Nearest Intersections Page Figure 7-63 Nearest NDB Page Select the Nearest NDB Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the second rectangular page icon. 2) Turn the small FMS Knob to select the third rectangular page icon.
SECTION 7 – NAVIGATION 7.12 NEAREST VOR 2) Press the ENT Key. The selected VOR frequency is placed in the NAV standby frequency field. 3) Press the FMS Knob to remove the flashing cursor. 7.13 NEAREST USER WAYPOINT Figure 7-64 Nearest VOR Page Select the Nearest VOR Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the fourth rectangular page icon.
SECTION 7 – NAVIGATION 2) Turn either FMS Knob to select the desired waypoint. The remaining information on the Nearest User Waypoint Page pertains to the selected Nearest User Waypoint. 2) Turn the FMS Knobs to select the desired facility or frequency. 3) Press the FMS Knob to remove the flashing cursor. 4) Press the FMS Knob to remove the flashing cursor. 7.14 NEAREST FREQUENCIES Figure 7-66 Nearest Frequencies Page Select the Nearest Frequencies Page 7.
SECTION 7 – NAVIGATION airspace and the current course takes the aircraft inside, ‘Ahead < 2 nm’ is displayed. • If the aircraft is within two nautical miles of an airspace and the current course will not take the aircraft inside, ‘Within 2 nm’ is displayed. • If the aircraft has entered an airspace, ‘Inside’ is displayed. View Additional Details for a Listed Airspace 1) With the Nearest Airspace Page displayed, press the FMS Knob to activate the cursor.
SECTION 7 – NAVIGATION Blank Page 7-32 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.
SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING 3) Turn the large FMS Knob to move the cursor to the next character field. The following discussions pertain to the Multi Function Display, unless otherwise indicated. 4) Repeat steps 2 and 3 until the desired name is entered. 8.1 5) Press the ENT Key. USER DEFINED WAYPOINTS 6) The cursor is now in the ‘REFERENCE WAYPOINTS’ field. If desired, the waypoint can be defined by a reference waypoint.
SECTION 8 – FLIGHT PLANNING Create User Waypoints from the Navigation Map Page 1) With the Navigation Map Page displayed, push the Joystick to activate the panning function. The target pointer is displayed at the present aircraft position. 2) Move the Joystick to place the pointer at the desired position 3) Press the ENT Key. The User Waypoint Information Page is now displayed with the captured position. 4) Turn the FMS Knobs to select a waypoint name. 5) Press the ENT Key to accept the selected name.
SECTION 8 – FLIGHT PLANNING turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. 8.4 ACTIVATE A FLIGHT PLAN LEG 1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired destination waypoint. 3) Turn the large FMS Knob to highlight ‘Delete Flight Plan’ and press the ENT Key. With ‘OK’ highlighted, press the ENT Key to deactivate the flight plan. This will not delete the stored flight plan, only the active flight plan.
SECTION 8 – FLIGHT PLANNING 8.7 CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the MFD 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Select the NEW Softkey to display a blank flight plan page for the first empty storage location. Figure 8-10 Create FPL on MFD Create a New Flight Plan Using the PFD NOTE: A flight plan cannot be entered using the PFD if another flight plan is active.
SECTION 8 – FLIGHT PLANNING 8.8 ENTER AN AIRWAY IN A FLIGHT PLAN 5) When the desired entry point is entered, press the ENT Key. 1) Press the FPL Key to display the active flight plan or display a stored flight plan. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the waypoint before which the airway will be entered. Figure 8-15 Airway Entry Point Loaded 6) Turn the small FMS Knob to display the Waypoint Information Window.
SECTION 8 – FLIGHT PLANNING Figure 8-19 Airway Added to Flight Plan 8.9 Figure 8-17 Select Desired Airway LOAD A DEPARTURE See the Procedures section for a discussion on loading and activating departure procedures. 8) Turn either FMS Knob to highlight the desired airway. 8.10 LOAD AN ARRIVAL 9) Press the ENT Key. A list of available exits is now displayed. See the Procedures section for a discussion on loading and activating arrival procedures.
SECTION 8 – FLIGHT PLANNING 8.13 STORE A FLIGHT PLAN 1) After creating a flight plan on either the PFD or MFD, it may be saved by pressing the MENU Key. 2) Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press the ENT Key. 3) With ‘OK’ highlighted, press the ENT Key to store the flight plan. Figure 8-20 Store Flight Plan Confirmation 8.14 EDIT A STORED FLIGHT PLAN 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page.
SECTION 8 – FLIGHT PLANNING 4) A ‘Copy to flight plan #?’ confirmation window is displayed. With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel, turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. 8.20 WEIGHT PLANNING NOTE: All weight planning page data fields displays data rounded to the nearest 10 pounds or 5 kilograms. 8.18 DELETE A FLIGHT PLAN 1) From the Flight Plan Catalog Page, press the FMS Knob to activate the cursor.
SECTION 8 – FLIGHT PLANNING Enter a Pilot and Stores Weight Enter Fuel on Board Weight: 1) Press the FMS Knob to activate the cursor and highlight the ‘PILOT AND STORES’ field. 1) Press the FMS Knob to activate the cursor and highlight the ‘FUEL ON BOARD’ field. 2) Turn the small FMS Knob to enter the pilot and stores weight. 2) Turn the small FMS Knob to enter the fuel on board. 3) Press the ENT Key to confirm the entry. 3) Press the ENT Key to confirm the entry.
SECTION 8 – FLIGHT PLANNING Weight Caution And Warning Conditions Starting WPT Ending WPT If the zero fuel weight is greater than the maximum allowable zero fuel weight, then the zero fuel weight is displayed in amber. If the aircraft weight is greater than the maximum allowable takeoff weight, then 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.
SECTION 8 – FLIGHT PLANNING For flight plan leg planning, select the FPL Softkey (at the bottom of the display) and turn the small FMS Knob to select the desired flight plan (already stored in memory), by number. Turn the large FMS Knob to highlight the ‘LEG’ field and turn the small FMS Knob to select the desired leg of the flight plan, or select ‘CUM’ to apply trip planning calculations to the entire flight plan. Selecting ‘FPL 00’ displays the active flight plan.
SECTION 8 – FLIGHT PLANNING Blank Page 8-12 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.
SECTION 9 – PROCEDURES SECTION 9: PROCEDURES 9.1 ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1) Press the PROC Key. 2) Turn the large FMS Knob to hightlight ‘SELECT DEPARTURE’. 3) Press the ENT Key. 4) If a flight plan is active, the departure airport is displayed as the default. A list of available departures is also displayed. If no flight plan is active, use the FMS Knobs to enter the identifier of the desired airport. Press the ENT Key.
SECTION 9 – PROCEDURES 7) A second window is displayed listing available transitions for the arrival. Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key. Figure 9-4 Select Arrival Transition 8) A third window is displayed listing the available runways. Turn either FMS Knob to select the desired runway and press the ENT Key. Figure 9-5 Select Arrival Runway 9) With ‘LOAD?’ highlighted, press the ENT Key.
SECTION 9 – PROCEDURES Load and/or Activate an Approach Procedure 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT APPROACH’. 3) Press the ENT Key. 4) If a flight plan is active, the destination airport is displayed as the default. A list of available approaches is also displayed. If no flight plan is active, use the FMS Knobs to enter the identifier of the desired airport. Press the ENT Key. 7) The cursor moves to the TRANSITIONS field.
SECTION 9 – PROCEDURES Blank Page 9-4 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.
SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1) With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. Turn the small FMS Knob to select the ‘Weather’ group (Figure 10-2) to customize the display of weather features. Select ‘Traffic’ to customize the display of traffic. 10.
SECTION 10 – HAZARD AVOIDANCE At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The presence of Stormscope lightning data is indicated by the annunciation ‘LTNG < 25 nm’ in the upper right corner. Figure 10-5 Lightning Display Range Annunciation Select ‘cell’ or ‘strike’ as the Stormscope lightning mode: 1) With the Weather Group selected, press the ENT Key. The cursor flashes on ‘STRMSCP LTNG’. 2) Turn the large FMS Knob to select ‘STRMSCP MODE’.
SECTION 10 – HAZARD AVOIDANCE Select the CLEAR Softkey to remove all Stormscope lightning data from the display. 10.3 XM WEATHER (OPTIONAL) WARNING: Use of XM weather for hazardous weather penetration is not recommended. Weather information provided by XM Radio Service is approved only for weather avoidance, not penetration. 1) From the Navigation Map Page, select the MAP Softkey.
SECTION 10 – HAZARD AVOIDANCE Displaying Weather on the Weather Data Link Page Select the Weather Data Link Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Weather Data Link Page. 3) Press the available softkeys to select the desired XM weather product. 4) Select the LEGEND Softkey to view the legends for the selected products. If necessary, turn either FMS Knob to scroll through the list. Press the small FMS Knob or the ENT Key to return to the map.
SECTION 10 – HAZARD AVOIDANCE CELL MOV – selecting the CELL MOV Softkey shows storm cell movement by displaying an arrow. pointing in the direction of predicted movement. The display is updated every 12 minutes. SIG/AIR – selecting the SIG/AIR Softkey shows SIGMET and AIRMET information. The display is updated every 12 minutes. METAR – select the METAR Softkey to graphically display METARs. METARS are shown as colored flags at airports providing METAR reports. The display is updated every 12 minutes.
SECTION 10 – HAZARD AVOIDANCE • County Warnings • Cyclone Warnings Echo Top (Cloud Top and Echo Top Mutually Exclusive) Figure 10-10 Weather Product Symbols The XM Information Page in the AUX Page Group displays the weather products available for the current subscription. A green box by the weather product means that it is available. NOTE: The LOCK Softkey on the AUX - XM INFORMATION page is used to save the GDL 69(A) activation data when the XM services are initially set up.
SECTION 10 – HAZARD AVOIDANCE 10.4 TRAFFIC ADVISORY SYSTEM (TAS) Displaying Traffic on the Traffic Map Page Refer to the Honeywell KTA 870 Pilot’s Guide for a detailed discussion of the KTA 870 system. 1) Turn the large FMS Knob to select the Map Page Group. System Self Test 2) Turn the small FMS Knob to select the second rectangular page icon. 1) Set the range to 2/6 nm. 2) Select the STANDBY Softkey. 3) Select the TEST Softkey. 4) Self test takes approximately eight seconds to complete.
SECTION 10 – HAZARD AVOIDANCE Operating Mode Altitude Mode Non-Threat Traffic “Non-Bearing” Traffic (System is Unable to Determine Bearing), Aircraft Distance is 8.0 nm, 1100’ Above and Descending Traffic Advisory, Offscale, Aircraft is Out of Range Proximity Traffic, Aircraft is 1700’ Above and Descending Non-Threat Traffic Traffic Advisory, Aircraft is 1200’ Above and Climbing Figure 10-12 Traffic Map Page Displaying Traffic on the Navigation Map 1) Ensure the KTA 870 system is operating.
SECTION 10 – HAZARD AVOIDANCE 10.5 TERRAIN AND OBSTACLE PROXIMITY NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. Displaying Terrain and Obstacles on the Terrain Proximity Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the last rectangular page icon. 3) If desired, select the VIEW Softkey to access the ARC and 360 Softkeys.
SECTION 10 – HAZARD AVOIDANCE Displaying Terrain and Obstacles on the Navigation Map 1) With the Navigation Map displayed, select the MAP Softkey. 2) Select the TERRAIN Softkey. Terrain and obstacle proximity is now be displayed on the map. 10.6 TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY (OPTIONAL) NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.
SECTION 10 – HAZARD AVOIDANCE Color Terrain/Obstacle Location Alert Level Red Terrain/Obstacle above or within 100’ below current aircraft altitude. WARNING Yellow Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. CAUTION Black Terrain/Obstacle is more than 1000’ below aircraft altitude. NO DANGER Potential Impact Point Projected Flight Path 100' Threshold Unlighted Obstacle 1000' Enable/Disable Aviation Data 1) While the TAWS Page is displayed, press the MENU Key.
SECTION 10 – HAZARD AVOIDANCE NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach, a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix. Manual System Test A system test is automatically performed at power-up. After sucessful completion of the test, “TAWS System Test, OK” is heard.
SECTION 10 – HAZARD AVOIDANCE Negative Climb Rate After Takeoff Alert (NCR) 500 400 300 “Too Low, Terrain” 200 100 Runway 1 Threshold 2 3 4 5 6 7 8 9 10 11 12 13 14 15 Distance From Destination Airport (nm) Figure 10-19 PDA Alerting Excessive Descent Rate Alert (EDR) The purpose of the Excessive Descent Rate alert is to provide suitable alerts when the aircraft is determined to be closing (descending) upon terrain at an excessive speed.
SECTION 10 – HAZARD AVOIDANCE Displaying Terrain and Obstacles on the Navigation Map 1) With the Navigation Map displayed, select the MAP Softkey. 2) Select the TERRAIN Softkey. Terrain and obstacle proximity is now displayed on the map.
SECTION 10 – HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
SECTION 10 – HAZARD AVOIDANCE The following system status annunciations may also be issued. PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Availble” will be heard when sufficient GPS signal is re-established.
SECTION 10 – HAZARD AVOIDANCE 10.7 AIRBORNE COLOR WEATHER RADAR Weather Radar Basics Antenna Beam Illumination It is important to understand the concept of the antenna beam illumination. The radar beam is much like the beam of a spotlight. The farther the beam travels, the wider it gets. The radar is only capable of “seeing” what is inside the boundaries of the beam. Altitude (x1000 ft.) 80 Antenna at Zero Tilt 0 15 Half Power at 18,000 ft. 9° 0 Figure 10-26 depicts a radar beam’s characteristics.
SECTION 10 – HAZARD AVOIDANCE Radar Signal Attenuation Attenuation because of distance is due to the fact that the radar energy leaving the antenna is inversely proportional to the square of the distance. The reflected radar energy from a target 40 miles away that fills the radar beam is one fourth the energy reflected from an equivalent target 20 miles away. This would appear to the operator that the storm is gaining intensity as the aircraft gets closer.
SECTION 10 – HAZARD AVOIDANCE Ground Returns The intensity of ground target returns depends upon the angle at which the radar beam strikes the ground target (Angle of Incidence) and the reflective properties of that target. The gain can be adjusted so shorelines, rivers, lakes, and cities are well-defined. Increasing gain too much causes the display to fill in between targets, thus obscuring some landmarks.
SECTION 10 – HAZARD AVOIDANCE Safe Operating Distance Basic Antenna Tilt Setup The zone in which the radiation level exceeds the US Government standard of 1 mW/cm2 is the semicircular area of at least 9.16 feet from the 10-inch antenna (Figure 10-30). All personnel must remain outside of this zone. With a scanning or rotating beam, the averaged power density at the Maximum Permissible Exposure Level (MPEL) boundary is significantly reduced. MPEL Boundary 9.
SECTION 10 – HAZARD AVOIDANCE Weather Mapping and Interpretation Weather Display Interpretation When evaluating various target returns on the weather radar display, the colors denote precipitation intensity and rates as shown in Figure 10-32. Weather Mode Color Intensity Approximate Precipitation Rate (in/hr.) BLACK < 23 dBZ < .01. GREEN 23 dBZ to < 32 dBZ .01 - 0.1. YELLOW 32 dBZ to < 41 dBZ 0.1 - 0.5 RED 41 dBZ to < 50 dBZ 0.
SECTION 10 – HAZARD AVOIDANCE Tornadoes There are no conclusive radar target return characteristics which identify a tornado. However, tornadoes may be present if the following characteristics are observed: • A narrow, finger-like portion (Figure 10-33) extends and in a short time curls into a hook and closes on itself.
SECTION 10 – HAZARD AVOIDANCE Displaying Weather on the Weather Radar Page 1) Select the Map Page Group. 2) Select the Weather Radar Page. 3) Select the MODE Softkey. 4) To select Weather Mapping Mode: a) While on the ground, select the STANDBY Softkey. A one-minute warm-up period is initiated (countdown is displayed on the screen). After the warm-up is complete, the radar enters the Standby Mode. Figure 10-36 Confirming Activating Radar b) When the aircraft is airborne, select the WEATHER Softkey.
SECTION 10 – HAZARD AVOIDANCE Vertically Scanning a Storm Cell NOTE: Vertical scanning of a storm cell should be done with the aircraft wings level to avoid constant adjustment of the Bearing Line. 1) While in the Horizontal Scan view, select the BRG Softkey. This places the cursor in the BEARING field and displays the Bearing Line (Figure 10-37). 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.
SECTION 10 – HAZARD AVOIDANCE Adjusting Antenna Tilt Angle Tilt Line In order to make an accurate interpretation of a storm cell, the radar beam should be pointed at the wet part of the weather cell to record the proper rainfall intensity (color level). The ideal aiming point is just below the freezing level of the storm. The best way to find this point is to use the Vertical Scan feature.
SECTION 10 – HAZARD AVOIDANCE Adjusting Gain WARNING: Changing the gain in weather mode causes precipitation intensity to be displayed as a color not representative of the true intensity. See Figures 10-40 and 10-41. Remember to return the gain setting to ‘Calibrated’ for viewing the actual intensity of precipitation. 1) Select the GAIN Softkey to activate the cursor in the GAIN field. 2) Turn the small FMS Knob to adjust the gain for the desirable level.
SECTION 10 – HAZARD AVOIDANCE 5) If desired, readjust the Bearing Line as discussed previously to change the center of the Sector Scan. 6) Select the BRG Softkey again to remove the Bearing Line and cursor. The bearing reference is also reset to 0º. Figure 10-42 Selecting Sector Scan Position 2) 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 Sector Scan.
SECTION 10 – HAZARD AVOIDANCE Weather Attenuated Color Highlight (WATCH™) While in horizontal scan mode, this feature can be used as a tool to determine areas of possible inaccuracies in displayed intensity due to weakening of the radar energy. This weakening is known as ‘attenuation’. Accuracy of the displayed intensity of returns located in the shaded areas are suspect. Proper antenna tilt management should still be employed to determine the extent of attenuation in a shaded area.
SECTION 10 – HAZARD AVOIDANCE used as a supplement to the navigation map on the MFD. Ground Map mode uses a different gain range than Weather mode. Different colors are also used to represent the intensity levels. The displayed intensity of ground target returns are defined in Figure 10-48. Use of the GAIN and TILT controls help improve contrast so that specific ground targets can be recognized more easily.
SECTION 10 – HAZARD AVOIDANCE Blank Page 10-30 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.
SECTION 11 – ADDITIONAL FEATURES SECTION 11: ADDITIONAL FEATURES 11.1 SAFETAXI When the map range is decreased to level sufficient to view airport detail, runways with numbers, taxiways with identifying letters/numbers, airport Hot Spots, and airport landmarks including ramps, buildings, control towers, and other prominent features are shown. When the aircraft location is within the screen boundary an airplane symbol is shown for enhanced position awareness.
SECTION 11 – ADDITIONAL FEATURES 3) Turn the FMS Knob to select the Aviation Group and press the ENT Key. Figure 11-3 Selecting the Aviation Group 4) Turn the large FMS Knob to scroll through the Aviation Group options to SAFETAXI. 5) Turn the small FMS Knob to display the range of distances. 6) Turn either FMS Knob to select the desired distance for maximum SafeTaxi display range. 7) Press the ENT Key to complete the selection. 8) Press the FMS Knob to return to the Navigation Map Page.
SECTION 11 – ADDITIONAL FEATURES 11.2 TERMINAL PROCEDURE CHARTS (OPTIONAL) When no terminal procedure chart is available, the banner CHART NOT AVAILABLE appears on the screen. The CHART NOT AVAILABLE banner does not refer to the Jeppesen subscription, but rather the availability of a particular airport chart selection or procedure for a selected airport.
SECTION 11 – ADDITIONAL FEATURES 4) Turn the small and large FMS Knob to enter the desired airport identifier. Chart Not To Scale 5) Press the ENT Key. 6) Turn 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) With the desired chart displayed, press the ENT Key.
SECTION 11 – ADDITIONAL FEATURES ChartView Selecting the CHRT OPT Softkey displays the next level of softkeys. Selecting the ALL Softkey shows the entire chart on the screen. Selecting the HEADER Softkey shows the header view (approach chart briefing strip) on the screen as seen in Figure 11-8. Figure 11-9 Plan View 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.
SECTION 11 – ADDITIONAL FEATURES Selecting the MINIMUMS Softkey displays the minimum descent altitude/visibility strip at the bottom of the approach chart. Figure 11-12 Options Menu 3) Turn the large FMS Knob to move the cursor to the COLOR SCHEME Options (Figure 11-13). Figure 11-11 Minimums View 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 fit the available screen width.
SECTION 11 – ADDITIONAL FEATURES 11.3 XM RADIO (OPTIONAL) XM Satellite Radio services are subscription-based. For more information on specific 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, depending on the equipment. Either the Audio Radio ID or the Data Radio ID, or both, must be provided to XM Satellite Radio to activate the entertainment subscription.
SECTION 11 – ADDITIONAL FEATURES Using XM Radio Selecting a Channel from the Channel List The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio. The Active Channel displays the currently selected channel that the XM Radio is using. The Channel List shows a list of the available channels for the selected category. Channels can be stepped through one at a time or may be selected directly by channel number.
SECTION 11 – ADDITIONAL FEATURES Turn the small FMS Knob to display the Categories list. Highlight the desired category with the small FMS Knob and press the ENT Key. Selecting All Categories places all channels in the list. 3) Select any one of the (PS1 - PS15) softkeys to assign a number to the active channel. 4) Select the SET Softkey on the desired channel number to save the channel as a preset. Selecting the BACK Softkey returns the system to the top level softkeys.
SECTION 11 – ADDITIONAL FEATURES Data Link Receiver Error Messages Message Message Location CHECK ANTENNA XM Radio Page - active channel field UPDATING XM Radio Page - active channel field XM Radio Page - active channel field Weather Datalink Page - center of page XM Radio Page - active channel field XM Radio Page - active channel field XM Radio Page - active channel field NO SIGNAL LOADING OFF AIR --- Description Data Link Receiver antenna error; service required Data Link Receiver updating encryption co
SECTION 11 – ADDITIONAL FEATURES 11.4 SCHEDULER The Scheduler feature can be used to enter and display reminder messages (e.g., Hot Section Inspection or Phase 1 Maintenance Check) in the Alerts Window on the PFD. Messages can be set to display based on a specific date and time (event), once the message timer reaches zero (one-time; default setting), or recurrently whenever the message timer reaches zero (periodic).
SECTION 11 – ADDITIONAL FEATURES 9) For event-based messages: a) Use the FMS Knob to enter the desired date (DDMM-YY) and press the ENT Key. b) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field. c) Use the FMS Knob to enter the desired time (HH: MM) and press the ENT Key. 10) Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message. Deleting a Scheduler Message 1) Select the AUX - Utility Page.
SECTION 12 – ABNORMAL OPERATION SECTION 12: ABNORMAL OPERATION 3) PFD2 – By pressing the DISPLAY BACKUP button on the right audio panel. 12.2 ABNORMAL COM OPERATION 12.1 REVERSIONARY MODE When a COM tuning failure is detected by the system, the emergency frequency (121.500 MHz) is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected. In the event of a dual display failure, the emergency frequency (121.
SECTION 12 – ABNORMAL OPERATION 12.3 UNUSUAL ATTITUDES The PFD ‘declutters’ when the aircraft enters an unusual attitude. Only the primary functions are displayed in these situations.
SECTION 12 – ABNORMAL OPERATION uses its last-known position combined with continuously updated airspeed and heading data (when available) to calculate and display the aircraft’s current estimated position. NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic (OCN) phase of flight. In all other phases, an invalid GPS solution produces a “NO GPS POSITION” annunciation on the map and the G1000 stops navigating in GPS Mode.
SECTION 12 – ABNORMAL OPERATION Blank Page 12-4 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.
SECTION 13 – ANNUNCIATIONS & ALERTS SECTION 13: ANNUNCIATIONS & ALERTS 13.1 CAS MESSAGES Warning Messages When a new red CAS warning message appears, it flashes (inversely red on white) in conjunction with the Master Warning Indicator. Pressing the Master Warning Indicator acknowledges all flashing red messages, extinguishing the master warning lights, and stops warning message flashing. Once acknowledged, CAS warning messages are shown in red text and are displayed until the issue is corrected.
SECTION 13 – ANNUNCIATIONS & ALERTS Caution Messages When a new yellow caution message appears on the CAS display, it flashes (inversely black on yellow). The 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.
SECTION 13 – ANNUNCIATIONS & ALERTS Messages Comments STALL HEAT ON STALL NO HEAT STARTER VACUUM LOW Stall warning heat on while engine off Stall warning heat off Starter generator running Vacuum pressure less than 3.
SECTION 13 – ANNUNCIATIONS & ALERTS 13.3 REVERSIONARY SENSOR ANNUNCIATIONS Reversionary Sensor Window Text Condition BOTH ON ADC1 Both PFDs are displaying data from the number one Air Data Computer. BOTH ON ADC2 Both PFDs are displaying data from the number two Air Data Computer. BOTH ON AHRS1 Both PFDs are displaying data from the number one Attitude & Heading Reference System. BOTH ON AHRS2 Both PFDs are displaying data from the number two Attitude & Heading Reference System.
SECTION 13 – ANNUNCIATIONS & ALERTS PFD/MFD TAWS Page Annunciation Alert Type Reduced Required Terrain Clearance Caution (RTC) MFD Map Page Pop-Up Alert Aural Message or “Caution, Terrain; Caution, Terrain” or “Terrain Ahead; Terrain Ahead” or “Terrain Ahead; Terrain Ahead” or “Caution, Terrain; Caution, Terrain” or “Caution, Obstacle; Caution, Obstacle” or “Obstacle Ahead; Obstacle Ahead” or “Obstacle Ahead; Obstacle Ahead” or “Caution, Obstacle; Caution, Obstacle” Imminent Terrain Impact Cauti
SECTION 13 – ANNUNCIATIONS & ALERTS 13.5 OTHER G1000 AURAL ALERTS Aural Alert Description “Minimums, minimums” The aircraft has descended below the preset barometric minimum descent altitude. “Vertical track” “Traffic” “Traffic not available” The aircraft is one minute from Top of Descent. Issued only when vertical navigation is enabled. The Traffic Information Service (TIS) has issued a Traffic Advisory alert The aircraft is outside the Traffic Information Service (TIS) coverage area. 13.
SECTION 13 – ANNUNCIATIONS & ALERTS A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 13-2 illustrates all possible flags and the responsible LRUs.
SECTION 13 – ANNUNCIATIONS & ALERTS System Annunciation Comment Indicates a configuration module failure. This annunciation is only be seen when the autopilot is engaged. The annunciation indicates an AHRS monitor has detected an abnormal flight parameter, possibly caused by strong turbulence. In this case, the situation should correct itself within a few seconds. If there is an actual failure, a red “X” will soon appear over the Attitude Indicator.
SECTION 13 – ANNUNCIATIONS & ALERTS System Annunciation Comment Display is not receiving valid heading input from AHRS. Display is not receiving valid transponder information. Other Various Red X Indications A red ‘X’ through any other display field, such as engine instrumentation fields, indicates that the field is not receiving valid data. MFD & PFD Message Advisories Message DATA LOST – Pilot stored data was lost. Recheck settings. XTALK ERROR – A flight display crosstalk error has occurred.
SECTION 13 – ANNUNCIATIONS & ALERTS MFD & PFD Message Advisories (Cont.) Message PFD1 COOLING – PFD1 has poor cooling. Reducing power usage. PFD2 COOLING – PFD2 has poor cooling. Reducing power usage. MFD1 COOLING – MFD1 has poor cooling. Reducing power usage. PFD1 KEYSTK – PFD1 [key name] Key is stuck. PFD2 KEYSTK – PFD2 [key name] Key is stuck. MFD1 KEYSTK – MFD [key name] Key is stuck. CNFG MODULE – PFD1 configuration module is inoperative. PFD1 VOLTAGE – PFD1 has low voltage.
SECTION 13 – ANNUNCIATIONS & ALERTS Database Message Advisories (Cont.) Message MFD1 DB ERR – MFD1 basemap database error exists. PFD1 DB ERR – PFD1 basemap database error exists. PFD2 DB ERR – PFD2 basemap database error exists. MFD1 DB ERR – MFD1 terrain database error exists. PFD1 DB ERR – PFD1 terrain database error exists. PFD2 DB ERR – PFD2 terrain database error exists. MFD1 DB ERR – MFD1 terrain database missing. PFD1 DB ERR – PFD1 terrain database missing.
SECTION 13 – ANNUNCIATIONS & ALERTS Database Message Advisories (Cont.) Message MFD1 DB ERR – MFD1 airport terrain database error exists. PFD1 DB ERR – PFD1 airport terrain database error exists. PFD2 DB ERR – PFD2 airport terrain database error exists. MFD1 DB ERR – MFD1 airport terrain database missing. PFD1 DB ERR – PFD1 airport terrain database missing. PFD2 DB ERR – PFD2 airport terrain database missing. MFD1 DB ERR – MFD1 Safe Taxi database error exists.
SECTION 13 – ANNUNCIATIONS & ALERTS Database Message Advisories (Cont.) Message DB MISMATCH – Terrain database type mismatch. DB MISMATCH – Obstacle database version mismatch. DB MISMATCH – Airport Terrain database mismatch. Comments The PFDs and MFD have different terrain database types installed. Install correct terrain database type in all displays. The PFDs and MFD have different obstacle database versions installed. Install correct obstacle database version in all displays.
SECTION 13 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories Message GIA1 CONFIG – GIA1 config error. Config service req’d. GIA2 CONFIG – GIA2 config error. Config service req’d. GIA1 CONFIG – GIA1 audio config error. Config service req’d. GIA2 CONFIG – GIA2 audio config error. Config service req’d. GIA1 COOLING – GIA1 temperature too low. GIA2 COOLING – GIA2 temperature too low. GIA1 COOLING – GIA1 over temperature. GIA2 COOLING – GIA2 over temperature. GIA1 SERVICE – GIA1 needs service.
SECTION 13 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message COM1 TEMP – COM1 over temp. Reducing transmitter power. COM2 TEMP – COM2 over temp. Reducing transmitter power. COM1 SERVICE – COM1 needs service. Return unit for repair. COM2 SERVICE – COM2 needs service. Return unit for repair. COM1 PTT – COM1 push-to-talk key is stuck. COM2 PTT – COM2 push-to-talk key is stuck. COM1 RMT XFR – COM1 remote transfer key is stuck. COM2 RMT XFR – COM2 remote transfer key is stuck.
SECTION 13 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message GPS1 SERVICE – GPS1 needs service. Return unit for repair. GPS2 SERVICE – GPS2 needs service. Return unit for repair. NAV1 SERVICE – NAV1 needs service. Return unit for repair. NAV2 SERVICE – NAV2 needs service. Return unit for repair. NAV1 RMT XFR – NAV1 remote transfer key is stuck. NAV2 RMT XFR – NAV2 remote transfer key is stuck. G/S1 FAIL – G/S1 is inoperative. G/S2 FAIL – G/S2 is inoperative.
SECTION 13 – ANNUNCIATIONS & ALERTS GTX 33 & GTX 33D Message Advisories Message XPDR1 CONFIG – XPDR1 config error. Config service req’d. XPDR2 CONFIG – XPDR2 config error. Config service req’d. MANIFEST – GTX1 software mismatch, communication halted. MANIFEST – GTX2 software mismatch, communication halted. XPDR1 SRVC – XPDR1 needs service. Return unit for repair. XPDR2 SRVC – XPDR2 needs service. Return unit for repair. XPDR1 FAIL – XPDR1 is inoperative. XPDR2 FAIL – XPDR2 is inoperative.
SECTION 13 – ANNUNCIATIONS & ALERTS GRS 77 Message Advisories (Cont.) Message AHRS1 GPS – AHRS1 not receiving backup GPS information. AHRS2 GPS – AHRS2 not receiving backup GPS information. AHRS1 GPS – AHRS1 operating exclusively in no-GPS mode. AHRS2 GPS – AHRS2 operating exclusively in no-GPS mode. AHRS MAG DB – AHRS magnetic model database version mismatch. AHRS1 SRVC – AHRS1 Magnetic-field model needs update. AHRS2 SRVC – AHRS2 Magnetic-field model needs update.
SECTION 13 – ANNUNCIATIONS & ALERTS GDL 69A Message Advisories Message GDL69 CONFIG – GDL 69 config error. Config service req’d. GDL69 FAIL – GDL 69 has failed. Comments GDL 69 configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. 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.
SECTION 13 – ANNUNCIATIONS & ALERTS GDC 74B Message Advisories (Cont.) Message MANIFEST – GDC1 software mismatch, communication halted. MANIFEST – GDC2 software mismatch, communication halted. Comments The GDC 74B has incorrect software installed. The G1000 system should be serviced. GCU 475 Message Advisories Message GCU CNFG – GCU Config error. Config service req’d. GCU FAIL – GCU is inoperative. MANIFEST – GCU software mismatch, communication halted. GCU KEYSTK – GCU [key name] Key is stuck.
SECTION 13 – ANNUNCIATIONS & ALERTS 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. This can also occur with user waypoints in a flight plan that is deleted.
SECTION 13 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Message Comments ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the aircraft position. than 2 nm. APR INACTV – Approach is not active. The system notifies the pilot that the loaded approach is not active. Activate approach when required. SLCT FREQ – Select appropriate The system notifies the pilot to load the approach frequency for the appropriate frequency for approach. NAV receiver.
SECTION 13 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Message STRMSCP FAIL – Stormscope has failed. FAILED PATH – A data path has failed. MAG VAR WARN – Large magnetic variance. Verify all course angles. SCHEDULER [#] – . ECS – Service required. CRUISE I – Cruise I conditions met. CRUISE II – Cruise II conditions met. EXCEEDANCE – Engine exceedance data is being logged. 190-00708-00 Rev. A Comments Stormscope has failed. The G1000 system should be serviced.
SECTION 13 – ANNUNCIATIONS & ALERTS Blank Page 13-24 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190-00708-00 Rev.
INDEX A Abnormal COM operation 12-1 Activate a flight plan 8-3 Activation Required 11-7 Active Channel 11-8, 11-9 Active flight plan 8-2 ADF 4-3 Advisory alerts 13-9 AFCS Status Box 2-1, 6-1 Age 10-6 AHRS 13-7 – 13-9, 13-17 – 13-20 Aircraft Symbol 6-3 AIRMET 10-5 Airport frequency 7-27 Airport information 7-23 Airspace alerts 7-30 Airspeed Indicator 2-1 Airspeed indicator 2-3 Airspeed Reference 6-9–6-10 Airspeed trend vector 2-3 Airways 1-12, 8-5 Air Data Computer 13-4 Alert messages 13-18, 13-19 Alert Pop-Up
INDEX Edit a flight plan 8-7 EDR 10-13 Electrical indications 3-2 Engine display 3-1 Essential bus voltage 3-1 Estimated Landing Fuel 8-9 Excessive Descent Rate 10-13 Excess Fuel Weight 8-9, 8-10 Glideslope Mode 6-15, 6-33 GMA 1347 1-1 Go Around Mode 6-16, 6-35–6-36 Ground mapping 10-29 H F Five-Hundred Aural Alert 10-13 Flap position 3-1 Asymmetrical deflection warning 3-8, 13-1 Flight director Modes, lateral 6-16–6-18 Modes, vertical 6-4–6-18 Flight Level Change Mode 6-9, 6-30, 6-32 Flight Plan Catalog 9
INDEX Navigation status window 2-2 NAV Frequency Window 4-1 NCR 10-13 Nearest Airports Page 7-23, 7-26, 7-28, 7-29, 7-30, 8-1 Nearest ARTCC & FSS frequencies 7-30 Negative Climb Rate After Takeoff 10-13 NEXRAD 1-8, 1-12, 10-3, 10-4, 10-5, 10-6 Non-path descent 6-32–6-33 Normal operating mode 12-1 O OBS 2-13 Obstacles 10-14, 13-12, 13-14 Oil, engine Alerts 3-8, 13-1 Pressure 3-1 Temperature 3-1 Operation 5-2 Optional NAV radios 4-3 Overspeed protection, autopilot 6-4 Oxygen Pressure 3-1 Warning 3-8, 13-1 P
INDEX T TAF 10-3 Takeoff Mode 6-16 TAS 10-7, 10-8, 10-22 – 10-27, 13-17 TAWS 10-10 – 10-12, 10-14 – 10-16, 13-4, 13-5 TAWS-B 10-10 TAWS system test 10-12 Terrain 1-7, 1-12, 10-9 – 10-12, 10-1 – 10-16, 12-2, 13-4, 13-5, 13-12 Terrain proximity 10-9 Tilt 10-25 Tilt line 10-25 TOD 7-16, 7-19 Topographical data 1-7, 1-12 Top of Descent 7-16 Tornado 10-5 Torque 3-1 Warning 3-8, 13-1 Track 2-1 Traffic 1-7, 1-12 Traffic advisory 10-7, 10-16, 10-22 Traffic map page 10-7, 10-8, 10-10, 10-14 Transponder 1-10, 4-4 Transp
Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p: 913.397.8200 f: 913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p: 503.391.3411 f: 503.364.2138 Garmin (Europe) Ltd 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.
