Garmin G1000 Socata TBM 850- User Manual

Garmin G1000 Socata TBM 850

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Table of Contents:

  • Page 2 – Garmin G1000 Pilot’s Guide for the Socata TBM 850
  • Page 3 – LIMITED WARRANTY
  • Page 4 – ii; WARNING; Aeronautical; Information
  • Page 5 – iii; NOTE
  • Page 6 – iv; REVISION INFORMATION; All
  • Page 7 – TABLE OF CONTENTS; SECTION 1 SYSTEM OVERVIEW
  • Page 8 – SECTION 5 FLIGHT MANAGEMENT
  • Page 9 – vii; SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM
  • Page 10 – viii; G1000 System Message Advisories; INDEX
  • Page 11 – SYSTEM OVERVIEW; SYSTEM DESCRIPTION; Refer to the AFCS section for details on the GFC 700 AFCS.
  • Page 12 – linked to both PFDs via HSDB connection.
  • Page 13 – both GIA 63Ws using an RS-485 digital interface.
  • Page 14 – DISPLAY BACKUP
  • Page 15 – communication with both PFDs.
  • Page 17 – Panel and AFCS sections respectively.; PFD CONTROLS; Figure 1-2 PFD Controls
  • Page 19 – CONTROLS ASSOCIATED WITH THE MFD; Dual FMS Knob
  • Page 20 – AFCS CONTROLS; With the exception of the; FD; and; SPD; Keys, if a key is selected, its respective annunciator is
  • Page 21 – ADDITIONAL AFCS CONTROLS; (Manual Electric Trim) Switch are additional AFCS
  • Page 22 – AUDIO PANEL CONTROLS; COM1 MIC
  • Page 23 – Press during play to play the previously recorded memory
  • Page 24 – SECURE DIGITAL CARDS; To; Figure 1-6 Display Bezel SD Card Slots; PFD
  • Page 25 – and emergency power supply operation.; Figure 1-7 PFD Initialization
  • Page 26 – SYSTEM OPERATION; NORMAL OPERATION; Figure 1-9 gives an example of the G1000 displays in normal mode.; Figure 1-9 Normal Operation; REVERSIONARY MODE; for further information regarding system-specific alerts.
  • Page 27 – DISPLAY BACKUP; Figure 1-11 DISPLAY BACKUP Button; AHRS OPERATION; Refer to the Appendices for specific AHRS alert information.
  • Page 28 – Air Data; Figure 1-13 AHRS Operation; Table 1-1 AHRS Operation Modes; GPS INPUT FAILURE
  • Page 29 – AIR DATA INPUT FAILURE; Figure 1-14 G1000 System Failure Annunciations
  • Page 30 – SOFTKEY FUNCTION; Softkey On; To select a softkey using the MFD Control Unit:; Press the center of the; SEL; Key to select the desired softkey.; PFD SOFTKEYS
  • Page 32 – Figure 1-16 Top Level PFD Softkeys
  • Page 33 – Figure 1-18 SENSOR Softkeys; Figure 1-19 PFD Configuration Softkeys; Figure 1-20 XPDR Softkeys
  • Page 34 – MFD SOFTKEYS
  • Page 35 – Figure 1-21 MFD Softkeys; GPS RECEIVER OPERATION; Use the large
  • Page 36 – To change the selected GPS receiver:; GPS; Or; MENU; Use the; FMS; Knob to highlight the receiver which is not selected and press the; ENT; The GPS Status Page provides the following information:
  • Page 37 – below the satellite signal accuracy measurements.; Predicting RAIM availability; Select the GPS Status Page.; RAIM
  • Page 39 – SBAS; MENUS; This options list
  • Page 40 – CLR; Figure 1-23 Page Menu Examples; MFD PAGE GROUPS; Figure 1-24 Page Title; placement of the current page within the group are indicated.; Selecting a page using the; large; Turn
  • Page 41 – Figure 1-26 Map Pages; service; Figure 1-27 Waypoint Pages; INFO
  • Page 42 – Figure 1-28 Auxiliary Pages; Figure 1-29 Nearest Pages
  • Page 43 – Figure 1-30 Flight Plan Pages
  • Page 44 – MFD SYSTEM PAGES; SYSTEM SETUP PAGE; Figure 1-32 System Setup Page
  • Page 45 – the following displayed data:
  • Page 46 – Affects aircraft weights on the Weight Planning Page.; • Class D
  • Page 47 – MFD D; GPS CDI
  • Page 48 – The GPS CDI Box on the System Setup Page displays the following:; COM C; COM frequency channel spacing.
  • Page 49 – Indicators and the altimeter barometric settings.
  • Page 51 – SYSTEM STATUS PAGE; Figure 1-34 Example System Status Page; The
  • Page 52 – DISPLAY BACKLIGHTING; AUTOMATIC ADJUSTMENT; also be adjusted from the MFD.; To adjust display backlighting manually:; Figure 1-35 Manual Display Backlighting Adjustment
  • Page 53 – To adjust key backlighting manually:; Figure 1-36 Manual Key Lighting Adjustment
  • Page 55 – FLIGHT INSTRUMENTS; SECTION 2 FLIGHT INSTRUMENTS; to the backup instruments.
  • Page 58 – FLIGHT INSTRUMENTS; AIRSPEED INDICATOR; Figure 2-4 Red Pointer; present for low speed awareness.
  • Page 60 – ATTITUDE INDICATOR; Figure 2-7 Attitude Indicator
  • Page 61 – Figure 2-9 Flight Director Format
  • Page 62 – ALTIMETER; Setting the Selected Altitude:; Turn the; ALT SEL; approach) up to the aircraft’s service ceiling.; Figure 2-12 Altimeter
  • Page 64 – Figure 2-14 Baro Sync Setting
  • Page 65 – Figure 2-15 Baro Transition Alert; RADAR ALTIMETER
  • Page 66 – Radar Height Range; Table 2-1 Radar Altimeter Sensitivity; Testing the Radar Altimeter:; SYSTEM; RA TEST; Figure 2-19 Radar Altimeter Test
  • Page 67 – VERTICAL DEVIATION; Figure 2-22 Glidepath Indicator
  • Page 68 – Changing the HSI display format:
  • Page 69 – Figure 2-25 Heading and Course Indications
  • Page 70 – Figure 2-27 Navigation Angle Settings
  • Page 71 – TURN RATE INDICATOR; Figure 2-28 Turn Rate Indicator and Trend Vector; BEARING POINTERS AND INFORMATION WINDOWS; Figure 2-29 HSI with Bearing and DME Information
  • Page 72 – • GPS-derived great circle distance to bearing source; DME INFORMATION WINDOW; DME radio installation is optional.
  • Page 73 – Figure 2-30 Course Deviation Indicator; CDI; Figure 2-31 Navigation Sources
  • Page 74 – Changing navigation sources:; Figure 2-32 Selecting a Navigation Source; accordingly when all of the following occur:
  • Page 75 – Figure 2-33 CDI Sync Setting
  • Page 76 – GPS CDI SCALING; Figure 2-34 GPS CDI Settings
  • Page 77 – Figure 2-35 Automatic CDI Scaling
  • Page 78 – Figure 2-36 Typical LNAV and LNAV+V Approach CDI Scaling; Figure 2-37 Typical LNAV/VNAV and LPV Approach CDI Scaling; • When a; conditions exist the color changes to yellow.; Table 2-2 Automatic GPS CDI Scaling
  • Page 79 – OBS MODE; OBS
  • Page 80 – Figure 2-39 Suspending Automatic Waypoint Sequencing
  • Page 81 – SUPPLEMENTAL FLIGHT DATA; Selecting the; DFLTS; TEMPERATURE DISPLAYS; Reversionary Mode; Figure 2-40 Outside Air Temperature; Normal Display
  • Page 82 – WIND DATA; Figure 2-41 Wind Data; No Data
  • Page 83 – Table 2-3 VNV Indication Removal Criteria
  • Page 84 – PFD ANNUNCIATIONS AND ALERTING FUNCTIONS; SYSTEM ALERTING; System. When a new message is issued, the
  • Page 85 – TRAFFIC ANNUNCIATION; • The PFD Inset Map is enabled, displaying traffic; TAWS ANNUNCIATIONS; Figure 2-44 Traffic and Example TAWS Annunciations
  • Page 86 – ALTITUDE ALERTING; XFR; Figure 2-45 PFD Selection Indications; Copilot-side Selected; The following occur when approaching the Selected Altitude:; Figure 2-46 Altitude Alerting Visual Annunciations; Deviation of ±200 feet; LOW ALTITUDE ANNUNCIATION; Figure 2-47 Low Altitude on GPS WAAS Approach; Altimeter
  • Page 87 – MINIMUM DESCENT ALTITUDE/DECISION HEIGHT ALERTING; Figure 2-48 Barometric MDA/DH Alerting Visual Annunciations; Altitude Reached
  • Page 88 – MARKER BEACON ANNUNCIATIONS; Figure 2-50 Marker Beacon Annunciations; Outer Marker
  • Page 89 – ABNORMAL OPERATIONS; ABNORMAL GPS CONDITIONS; Annunciation; LOI; Table 2-4 Abnormal GPS Conditions Annunciated on HSI; source) and the following items on the PFD to be shown in yellow:
  • Page 90 – UNUSUAL ATTITUDES; Figure 2-52 Pitch Attitude Warnings; Nose Low
  • Page 91 – ENGINE & AIRFRAME SYSTEMS; SECTION 3 ENGINE AND AIRFRAME SYSTEMS; Refer to the Pilot’s Operating Handbook (POH) for limitations.; Figure 3-1 Multi Function Display; EICAS Display
  • Page 92 – CAS messages appear in; EIS; Figure 3-2 Reversionary Mode
  • Page 94 – ENGINE PARAMETERS; TORQUE GAUGE; Figure 3-5 Torque Gauge; Maximum Climb Torque; PROPELLER RPM GAUGE; Figure 3-6 Propeller RPM Gauge
  • Page 95 – GENERATOR SPEED GAUGE; generator speed exceeds 104% a warning condition occurs.; Figure 3-7 Generator Speed Gauge; ITT GAUGE; Figure 3-8 Interturbine Temperature Gauge Status Annunciations; Engine Start; OIL PRESSURE AND TEMPERATURE GAUGES; Figure 3-9 Oil Pressure and Temperature Gauges
  • Page 96 – CABIN PRESSURIZATION; Figure 3-10 Cabin Pressure Display; normal display conditions.; FUEL INFORMATION; Figure 3-11 Fuel Display
  • Page 97 – ELECTRICAL INFORMATION; Figure 3-12 Electrical Display; TRIM AND FLAP INDICATORS; Figure 3-13 Trim and Flap Indications
  • Page 98 – Figure 3-14 Synoptic Pages Softkeys
  • Page 99 – ELECTRICAL SYSTEM; Figure 3-15 Electrical Synoptics Page
  • Page 100 – Switch Open; Main; Table 3-1 Generator Switch Status; A red “X” over a component indicates invalid data or a failed unit.
  • Page 101 – FUEL SYSTEM; Figure 3-17 Fuel Synoptics Page
  • Page 102 – A red “X” over a component indicated invalid data or a failed unit.; GENERAL SYSTEMS; • White indicates that heat is off (propeller and windshield); Figure 3-18 General Synoptics Page
  • Page 103 – CAS; Figure 3-19 CAS Messages
  • Page 104 – CAS MESSAGES AND PRIORITIZATION; Warning; Table 3-3 Warning CAS Messages
  • Page 105 – Inhibits; X X X; for example; Table 3-4 Caution CAS Messages
  • Page 106 – CAS DISPLAY INHIBITS; Activation; * Stored in terrain database
  • Page 107 – AUDIO PANEL AND CNS; SECTION 4 AUDIO PANEL AND CNS; • MFD Control Unit; AUDIO PANEL VOLUME CONTROL
  • Page 108 – PFD CONTROLS AND FREQUENCY DISPLAY
  • Page 109 – – Transfers the standby and active NAV frequencies.
  • Page 110 – Figure 4-2 Audio Panel Controls
  • Page 112 – COM TRANSCEIVER SELECTION AND ACTIVATION; COM transceiver state prior to shutdown.; Figure 4-3 Selecting a COM Radio for Transmit
  • Page 113 – TRANSMIT/RECEIVE INDICATIONS; COM MIC; Figure 4-4 COM Radio Transmit and Receive Indications; copilot has transmit priority on COM2.; COM TRANSCEIVER MANUAL TUNING; Manually tuning a COM frequency:; Frequency Transfer; Figure 4-5 COM Frequency Tuning
  • Page 114 – SELECTING THE RADIO TO BE TUNED; Press the small; Figure 4-6 Switching COM Tuning Boxes; COM; Knob to; Pressing and holding the COM; Press for Two Seconds to
  • Page 115 – AUTO-TUNING THE COM FREQUENCY; COM frequencies can be automatically tuned from the following:; AUTO-TUNING FROM THE PFD; Frequency; NRST; Softkey to Open
  • Page 116 – AUTO-TUNING FROM THE MFD; page group by highlighting the frequency and pressing the; Figure 4-9 Frequency Auto-Tuning from the MFD
  • Page 117 – Figure 4-10 Nearest Pages Menus; Nearest Airspaces Menu
  • Page 120 – FREQUENCY SPACING; Figure 4-13 COM Channel Spacing; Spacing; Figure 4-14 AUX – System Setup Page; COM Frequency
  • Page 121 – AUTOMATIC SQUELCH; Knob. When Automatic; Figure 4-15 Overriding Automatic Squelch; VOLUME; COM radio volume level can be adjusted from 0 to 100% using the; Figure 4-16 COM Volume Level
  • Page 122 – NAV RADIO SELECTION AND ACTIVATION; Figure 4-17 Selecting a NAV Radio for Navigation
  • Page 123 – ADF; Figure 4-18 Selecting a NAV Radio Receiver; NAV RECEIVER MANUAL TUNING; Manually tuning a NAV frequency:; Figure 4-19 NAV Frequency Tuning; NAV
  • Page 124 – Figure 4-20 Switching NAV Tuning Boxes; Figure 4-21 NAV Radio ID Indication; Figure 4-22 NAV Volume Levels
  • Page 125 – AUTO-TUNING A NAV FREQUENCY FROM THE MFD
  • Page 126 – Figure 4-24 Nearest Pages Menus; Nearest VOR Menu
  • Page 127 – VOR; FREQ
  • Page 128 – NRST – Nearest Airports Pages
  • Page 129 – AUTO-TUNING NAV FREQUENCIES ON APPROACH ACTIVATION; to a NAV frequency field as follows:
  • Page 130 – MARKER BEACON RECEIVER; Figure 4-27 Marker Beacon Annunciations on the PFD; HI SENS
  • Page 132 – ADF TUNING; Pressing the
  • Page 133 – SELECTING ADF RECEIVER MODE; Key on; Figure 4-32 Selecting ADF Receiver Mode; is set to 50%. The ADF volume level is the same for both Audio Panels.
  • Page 134 – DME TUNING; and the NAV1; DME; Selecting DME transceiver pairing:
  • Page 135 – TRANSPONDER CONTROLS
  • Page 136 – Selecting and activating Transponder 1 or Transponder 2:; TRANSPONDER MODE SELECTION; Selecting a transponder mode:
  • Page 137 – GROUND MODE; by selecting the; GND; Figure 4-36 Ground Mode; In Standby Mode, the IDENT function is inhibited.; Code Number and; Figure 4-37 Standby Mode; MANUAL ON MODE; ON Mode can be selected at any time by selecting the; ON Mode
  • Page 138 – selected manually by selecting the; ALT Mode; Figure 4-39 Altitude Mode; REPLY STATUS; reply status field of the Transponder Data Box.; Reply to; Figure 4-40 Reply Indication
  • Page 139 – ENTERING A TRANSPONDER CODE; Figure 4-41 Entering a Code; Figure 4-42 Entering a Code with the FMS Knob
  • Page 140 – VFR CODE; Figure 4-43 VFR Code; IDENT FUNCTION; In Standby Mode, the; Softkey is inoperative.; IDENT
  • Page 141 – FLIGHT ID REPORTING; center for configuration.; Flight ID
  • Page 142 – ADDITIONAL AUDIO PANEL FUNCTIONS; Stereo headsets are recommended for use in this aircraft.; SPEAKER; Each Audio Panel controls a separate cabin speaker. Pressing the; Figure 4-46 Music and Speaker Keys
  • Page 143 – INTERCOM; Figure 4-47 Intercom Controls
  • Page 144 – A passenger address system is provided by pressing the; Figure 4-48 PA Key Selected for Cabin Announcements; PA Key is Selected on; SIMULTANEOUS COM OPERATION
  • Page 145 – CLEARANCE RECORDER AND PLAYER; PLAY; Key; Figure 4-49 Clearance Recorder PLAY Key
  • Page 146 – ENTERTAINMENT INPUTS; can be adjusted by a Garmin-authorized service center.; MUSIC 1; MUSIC 1 M; MUSIC; MUSIC
  • Page 147 – AUDIO PANELS PREFLIGHT PROCEDURE; When the; MAN SQ; Figure 4-50 Audio Panel Controls
  • Page 148 – Setting the Audio Panels during preflight:; Figure 4-51 Radio and Headphone Volume Controls
  • Page 149 – ABNORMAL OPERATION; associated equipment, including switches and external devices.; STUCK MICROPHONE; Figure 4-52 Stuck Microphone Alert; COM TUNING FAILURE; Figure 4-53 COM Tuning Failure; Emergency Channel
  • Page 150 – PFD FAILURE, DUAL SYSTEM; Figure 4-54 Frequency Section of PFD2 Display after PFD1 Failure; Figure 4-55 PFD1 Display after PFD2 Failure
  • Page 151 – AUDIO PANEL FAIL-SAFE OPERATION; The red; Figure 4-56 Reversionary Mode Button
  • Page 153 – FLIGHT MANAGEMENT; the Pilot’s Guide explains GPS navigation using the G1000.
  • Page 154 – Figure 5-1 GPS Navigation Information on the PFD
  • Page 155 – NAVIGATION STATUS BOX; PFD Navigation Status Box; or; MFD Navigation Status Box; Changing a field in the MFD Navigation Status Box:; Select the System Setup Page.; Knob momentarily to activate the flashing cursor.
  • Page 156 – Turn the small; Knob to display and scroll through the data options list.; Softkey returns any field to its default setting.; USING MAP DISPLAYS; MAP ORIENTATION; Figure 5-3 Map Orientation
  • Page 157 – show the map orientation nor the wind direction and speed.; Figure 5-4 Navigation Map Page Menu Window; Map Setup
  • Page 158 – Figure 5-5 Map Setup Menu Window - Map Group; Orientation Field; MAP RANGE; Joystick; Figure 5-6 Map Range
  • Page 159 – AUTO ZOOM
  • Page 160 – Manual Range Override
  • Page 161 – MAP PANNING; Figure 5-8 Navigation Map - Map Pointer Activated; Map Pointer
  • Page 162 – Figure 5-9 Navigation Map - Map Pointer on Point of Interest; Map Pointer on
  • Page 163 – Figure 5-10 Navigation Map - Map Pointer on Airspace; to display the Map Pointer.; to move the Map Pointer around the map.
  • Page 164 – Place the Map Pointer on a waypoint.; NAVAID
  • Page 165 – Airspace
  • Page 166 – MEASURING BEARING AND DISTANCE; Figure 5-13 Navigation Map - Measuring Bearing and Distance; Measurement
  • Page 167 – TOPOGRAPHY; TOPO Off; TOPO On; TOPO
  • Page 168 – Figure 5-15 Navigation Map Setup Menu - TOPO DATA Setup; TOPO DATA
  • Page 169 – Figure 5-17 Navigation Map Setup Menu - TOPO SCALE Setup
  • Page 170 – MAP SYMBOLS; DCLTR; LAND SYMBOLS; The following items are configured on the land menu:; Off; Table 5-1 Land Symbol Information
  • Page 171 – AVIATION SYMBOLS; The following items are configured on the aviation menu:; Active Flight Plan Waypoint (ACTIVE FPL WPT); Table 5-2 Aviation Symbol Information
  • Page 172 – SYMBOL SETUP; Figure 5-18 Navigation Map Setup Menu - TOPO SCALE Setup; LAND DATA
  • Page 173 – Key to accept the selected range.; Knob to return to the Navigation Map Page.; Figure 5-19 Navigation Map Setup Menu - LAND GROUP Setup; Figure 5-20 Navigation Map Setup Menu - AVIATION GROUP Setup; Maximum Display Range
  • Page 174 – MAP DECLUTTER; The declutter level is displayed in the; Figure 5-21 Navigation Map - Declutter Level Indications; Declutter Level; Navigation Map Page Menu
  • Page 175 – various levels of declutter.; Table 5-3 Navigation Map Items Displayed by Declutter Level
  • Page 176 – AIRWAYS; Figure 5-22 Airways on MFD Navigation Page; Low Altitude
  • Page 177 – AIRWAY; Figure 5-23 Navigation Map Setup Menu - AIRWAYS Setup; Airway Display Selection
  • Page 178 – The following range items are configurable on the airways menu:; Table 5-4 Airway Range Information; TRACK VECTOR; Figure 5-24 Navigation Map -Track Vector; Track Vector
  • Page 179 – WIND VECTOR; Figure 5-26 Navigation Map - Wind Vector; Wind Direction
  • Page 180 – NAV RANGE RING; Figure 5-27 Navigation Map - Nav Range Ring; Nav Range Ring
  • Page 181 – FUEL RANGE RING; Figure 5-28 Navigation Map - Fuel Range Ring; Fuel Range Ring
  • Page 182 – used for all phases of flight planning and navigation.; Figure 5-29 Waypoint Information Window; to turn the small
  • Page 183 – Figure 5-30 Waypoint Information Window - Duplicate Identifier; Duplicate Message; AIRPORTS
  • Page 184 – Figure 5-31 Airport Information Page
  • Page 185 – View a destination airport:; From the Airport Information Page press the; Key. Select ‘View Destination Airport’. The Destination; * May include Additional Information; Table 5-5 Airport Frequency Abbreviations; Figure 5-32 Nearest Airports Window on PFD
  • Page 186 – Figure 5-33 Airport Information Window on PFD; Airport Information
  • Page 187 – Figure 5-34 Nearest Airport Page; LD APR
  • Page 188 – Figure 5-35 System Setup Page - Nearest Airport Selection Criteria; Nearest Airport Criteria
  • Page 189 – INTERSECTIONS; used to define the intersection.; Figure 5-36 Intersection Information Page
  • Page 190 – The list only includes waypoints that are within 200 nm.; Figure 5-37 Nearest Intersections Page
  • Page 191 – NDB; Figure 5-38 NDB Information Page
  • Page 192 – Figure 5-39 Nearest NDB Page
  • Page 193 – Figure 5-40 VOR Information Page; TERMINAL; Highlight ‘SELECT VOR WINDOW’, and press the
  • Page 194 – Knob to remove the flashing cursor.; Figure 5-41 Nearest VOR Page
  • Page 195 – USER WAYPOINTS; Figure 5-42 User Waypoint Information Page
  • Page 196 – Figure 5-43 Nearest User Waypoint Page; CREATING USER WAYPOINTS
  • Page 197 – Figure 5-44 User Waypoint Information Page Menu; the; EDITING USER WAYPOINTS
  • Page 199 – DELETING USER WAYPOINTS
  • Page 200 – Figure 5-45 Airspaces
  • Page 202 – Figure 5-46 System Setup Page - Airspace Alerts
  • Page 203 – Figure 5-47 Nearest Airspaces Page; ALERTS
  • Page 204 – Pressing the PFD; MSG; displayed in the message window:; Table 5-6 PFD Airspace Alert Messages
  • Page 205 – The Direct-to method of navigation, initiated by pressing the; Location of Destination
  • Page 206 – Activation Command; Figure 5-50 Waypoint Submenu; Waypoint Submenu
  • Page 208 – Page Menu
  • Page 210 – Removing a VNV altitude constraint:; With ‘Clear Vertical Constraints’ highlighted, press the; Figure 5-52 Direct-to Window - Clearing Vertical Constraints
  • Page 211 – Flight Plan Leg Type; Table 5-7 Flight Plan Leg Symbols
  • Page 212 – The following could cause the airway update to fail:; FLIGHT PLAN CREATION; There are three methods to create or modify a flight plan:; Figure 5-53 Active Flight Plan Page
  • Page 213 – Figure 5-54 Active Flight Plan Window on PFD; Creating an active flight plan:; FPL
  • Page 215 – ADDING WAYPOINTS TO AN EXISTING FLIGHT PLAN; Figure 5-56 Stored Flight Plan Page; Stored Flight Plan Selected; Softkeys; Figure 5-57 Active Flight Plan Page - FPL Full; Flight Plan Full Message
  • Page 216 – Figure 5-58 Duplicate Waypoints Window
  • Page 217 – ADDING AIRWAYS TO A FLIGHT PLAN; Figure 5-59 Select Airway Page - Selecting Airway
  • Page 218 – Figure 5-60 Select Airway Page - Selecting Exit Point
  • Page 219 – Figure 5-61 Active Flight Plan Page - Airway Inserted; Inserted Airway Header; RESTRICTIONS ON ADDING AIRWAYS; • Starting from AMANO, the airway can be flown only to LIBRO.
  • Page 220 – ADDING PROCEDURES TO A STORED FLIGHT PLAN; Figure 5-62 Stored Flight Plan Page; Flight Plan Name
  • Page 221 – Figure 5-63 Departure Loading Page - Selecting the Departure
  • Page 222 – Figure 5-64 Departure Loading Page - Selecting Transition
  • Page 223 – Figure 5-66 Arrival Loading Page - Selecting the Arrival
  • Page 224 – Figure 5-67 Arrival Loading Page - Selecting the Transition
  • Page 225 – Figure 5-69 Approach Loading Page - Selecting the Approach
  • Page 226 – Figure 5-70 Approach Loading Page - Selecting the Transition; FLIGHT PLAN STORAGE
  • Page 227 – Figure 5-72 Stored Flight Plan Information
  • Page 228 – SORT FLIGHT PLANS
  • Page 229 – DELETE A STORED FLIGHT PLAN; FLIGHT PLAN EDITING; navigation as soon as they are entered.; DELETING THE ACTIVE FLIGHT PLAN
  • Page 230 – DELETING FLIGHT PLAN ITEMS
  • Page 232 – ALONG TRACK OFFSETS
  • Page 233 – Figure 5-73 Along Track Offset
  • Page 234 – PARALLEL TRACK; Figure 5-74 Active Flight Plan Window - Selecting Parallel Track; Selecting Parallel
  • Page 235 – Figure 5-75 Parallel Track Window
  • Page 236 – Figure 5-77 Parallel Track Unavailable; Subdued Prompt; Figure 5-78 Cancelling Parallel Track; Cancel Prompt
  • Page 237 – ACTIVATING A FLIGHT PLAN LEG; Current
  • Page 238 – Figure 5-80 Active Flight Plan Page - New Active Leg; New Active; Confirmation Window; INVERTING A FLIGHT PLAN
  • Page 239 – FLIGHT PLAN VIEWS; Figure 5-81 Active Flight Plan - Leg to Leg vs. Cumulative Distance
  • Page 240 – WIDE; COLLAPSING AIRWAYS
  • Page 241 – CLOSEST POINT OF FPL
  • Page 242 – VERTICAL NAVIGATION; Figure 5-84 Enabling/Disabling Vertical Navigation; Current Vertical Navigation Profile; ENBL VNV; CNCL VNV
  • Page 243 – constraint “designated” for vertical guidance. Selecting the; Figure 5-85 Vertical Navigation Direct-To; VNV PROF
  • Page 244 – ALTITUDE CONSTRAINTS; Figure 5-86 Waypoint Altitude Constraints
  • Page 245 – Table 5-8 Altitude Constraint Size and Color Coding
  • Page 246 – An altitude constraint is invalid if:
  • Page 248 – DEPARTURES; LOADING A DEPARTURE INTO THE ACTIVE FLIGHT PLAN; PROC
  • Page 249 – Figure 5-87 Departure Selection
  • Page 250 – REMOVING A DEPARTURE FROM THE ACTIVE FLIGHT PLAN
  • Page 251 – ARRIVALS; LOADING AN ARRIVAL INTO THE ACTIVE FLIGHT PLAN; Figure 5-89 Arrival Selection; Destination Airport
  • Page 252 – Figure 5-90 Arrival Loading; Loaded Arrival
  • Page 253 – REMOVING AN ARRIVAL FROM THE ACTIVE FLIGHT PLAN; APPROACHES
  • Page 254 – HSI Annunciation; LNAV; Approach Type; LPV; Table 5-9 Approach Types; LOADING AN APPROACH INTO THE ACTIVE FLIGHT PLAN
  • Page 255 – Figure 5-91 Approach Selection
  • Page 256 – ACTIVATING AN APPROACH
  • Page 257 – REMOVING AN APPROACH FROM THE ACTIVE FLIGHT PLAN; MISSED APPROACH
  • Page 258 – COURSE TO FIX; Figure 5-93 Course to Fix; Course to Fix Waypoint
  • Page 259 – TRIP PLANNING; located in the AUX Page Group.; Figure 5-94 Trip Planning Page
  • Page 260 – TRIP STATISTICS
  • Page 261 – FUEL STATISTICS; by dividing the amount of fuel on board by the current fuel flow.; OTHER STATISTICS; Figure 5-95 Trip Planning Page - Flight Plan Mode; Starting and Ending Waypoint of; Figure 5-96 Trip Planning Page - Waypoint Mode; Selected Starting and Ending Waypoints
  • Page 262 – plan and leg selection.
  • Page 263 – WEIGHT PLANNING; Figure 5-97 Weight Planning Page; A/C Payload Calculator; Fuel On Board Sync Softkey
  • Page 264 – invalid values consisting of six dashes:
  • Page 265 – WEIGHT CAUTION AND WARNING CONDITIONS
  • Page 266 – RAIM PREDICTION; Figure 5-98 RAIM Prediction; Predicting RAIM availability at a selected waypoint:; Knob. The RAIM Prediction ‘WAYPOINT’ field is highlighted.
  • Page 267 – RAIM PREDICTION Box as follows:
  • Page 268 – can be enabled or disabled manually on the GPS Status Page.
  • Page 269 – Knob. The SBAS SELECTION ‘WAAS’ field is highlighted.; Key to disable SBAS. Press the; Key again to enable SBAS.
  • Page 270 – NAVIGATING A FLIGHT PLAN; should be considered not current.
  • Page 271 – Enter V4 into the flight plan.; Knob to activate the cursor.
  • Page 272 – The desired entry point for V4 (TOP) must be entered. Turn the large; Knob to highlight the desired flight; Figure 5-103 Begin Adding V4 to the Flight Plan; Figure 5-104 Entering V4 Entry Point
  • Page 273 – Figure 5-105 TOP Inserted into the Flight Plan
  • Page 274 – Figure 5-107 List of Available Exits for V4; If necessary, turn either; Press the
  • Page 275 – Figure 5-109 V4 is Loaded in the Flight Plan; Figure 5-110 Comfirm Active Leg
  • Page 276 – Verify the displayed leg is the desired leg and press the; No
  • Page 277 – Figure 5-112 Turn on to Active Leg
  • Page 278 – As seen in Figure 5-114, V244 is now the active flight plan leg.
  • Page 279 – Figure 5-115 HYS to LAA Leg Active; Figure 5-116 Direct To OPSHN
  • Page 280 – Turn the large; Figure 5-117 Enter VNV Altitude; An altitude of 10,000 feet is entered as requested by ATC.; Figure 5-118 Enter VNV Offset Distance
  • Page 282 – ‘SELECT APPROACH’ should be highlighted as shown in Figure 5-120.; Figure 5-120 Proceudures Window; Figure 5-121 List of Available Approaches; Turn either
  • Page 283 – Figure 5-122 List of Available Transitions; With ‘LOAD?’ highlighted, again press the; Key. The selected approach is added to the flight plan as seen; Figure 5-123 Loaded Approach
  • Page 284 – Figure 5-124 Designate HABUK Altitude Constraint; Figure 5-125 Designate FALUR Altitude Constraint
  • Page 285 – Figure 5-126 Vertical Guidance is Active to the FAF
  • Page 286 – Knob; Knob to enter the desired value.; Figure 5-127 Adjusting the Descent
  • Page 287 – Required Vertical
  • Page 288 – Figure 5-130 VDI & RVSI Showing Correctly Established Descent; Align Actual Vertical Speed
  • Page 289 – Figure 5-132 Turn to intercept OPSHN to FSHER Leg
  • Page 290 – Figure 5-133 Tracking the OPSHN to FSHER Leg
  • Page 291 – Figure 5-134 Approaching PYNON
  • Page 292 – Figure 5-135 Approach is Now Active; Figure 5-136 Manually Activate Approach
  • Page 293 – The aircraft altitude is 9,000 feet upon reaching HABUK.; Figure 5-137 Descending Turn to the Initial Approach Fix (IAF)
  • Page 294 – Figure 5-138 Descending to the FAF
  • Page 295 – Figure 5-139 Descending to the Missed Approach Point; ’. Again, if the aircraft altitude is lower than this prescribed
  • Page 296 – suspended past the MAP. Select the; Figure 5-140 Missed Approach Active
  • Page 297 – Figure 5-141 Establishing the Holding Pattern
  • Page 298 – ABNORMAL OPERATION
  • Page 299 – Figure 5-143 Dead Reckoning Mode - GPS Derived Data Shown in Yellow; or when a 65° bank angle is reached.
  • Page 301 – HAZARD AVOIDANCE; SECTION 6 HAZARD AVOIDANCE; Weather; XM SATELLITE WEATHER; use to penetrate hazardous weather.; ACTIVATING XM SATELLITE SERVICES
  • Page 303 – USING XM SATELLITE WEATHER PRODUCTS; Viewing the Weather Data Link Page:; Knob to select the Map Page Group.; Knob to select the Weather Data Link Page.; Figure 6-2 Weather Data Link Page
  • Page 304 – Weather Product; Table 6-1 Weather Product Symbols and Data Timing
  • Page 305 – NEXRAD; Table 6-2 Weather Product Display Maps
  • Page 306 – WEATHER SOFTKEYS ON THE WEATHER DATA LINK PAGE; Figure 6-3 Weather Softkeys
  • Page 307 – Figure 6-4 Page and Map Setup Menus; Data Link Setup Menu
  • Page 308 – Figure 6-6 Navigation Map Page Setup Menu
  • Page 309 – Figure 6-8 Panning on the Weather Data Link Page
  • Page 310 – Figure 6-9 NEXRAD Data on the Weather Data Link Page
  • Page 311 – Displaying NEXRAD weather information:; MAP; Softkey (for the PFD Inset Map, select the; INSET; Softkey). This step is not necessary on the; LEGEND; No Radar; Figure 6-10 NEXRAD Data with Legend
  • Page 312 – NEXRAD L; NEXRAD radar images may have certain limitations:; Each block
  • Page 313 – • Ground clutter; • Radar coverage extends to 55oN.; Precipitation
  • Page 314 – ECHO TOPS; Figure 6-13 Echo Tops Data
  • Page 315 – Displaying Echo Tops information:; Select the Weather Data Link Page with the; To display the Echo Tops legend, select the; Figure 6-14 ECHO TOPS Legend
  • Page 316 – CLOUD TOPS; Cloud Tops and Echo Tops cannot be displayed at the same time.; Figure 6-15 Cloud Tops Data; Displaying Cloud Tops information:; CLD TOP; To display the Cloud Tops legend, select the; Figure 6-16 Cloud Tops Legend
  • Page 317 – XM LIGHTNING; XM Lightning and optional L-3 STORMSCOPE; Lightning; Figure 6-17 Lightning Data
  • Page 318 – Displaying XM Lightning information:; XM LTNG; Figure 6-18 Lightning Legend; CELL MOVEMENT; Figure 6-19 Cell Movement Data; Storm
  • Page 319 – Figure 6-20 Cell Movement Legend; SIGMETS AND AIRMETS; Convective
  • Page 320 – Displaying SIGMETs and AIRMETs:; To display the SIGMET and AIRMET legend, select the; Sample SIGMET Text; Figure 6-22 SIGMET/AIRMET Text and Legend
  • Page 321 – METARS AND TAFS; Figure 6-23 METAR Flags on the Weather Data Link Page
  • Page 322 – Figure 6-24 METAR with Text; Figure 6-25 METAR Legend
  • Page 323 – SURFACE ANALYSIS AND CITY FORECAST
  • Page 324 – Figure 6-27 Surface Analysis Legend; FREEZING LEVEL; Figure 6-28 Freeze Level Data
  • Page 325 – To display the Freezing Level legend, select the; Figure 6-29 Freezing Level Legend; WINDS ALOFT
  • Page 326 – To display the Winds Aloft legend, select the; Figure 6-31 Winds Aloft Data with Legend
  • Page 327 – COUNTY WARNINGS; Figure 6-32 County Flood and Thunderstorm Warnings; Thunderstorm; Displaying County Warning information:; MORE WX; COUNTY; To display the County Warnings legend, select the; Figure 6-33 County Warnings Legend
  • Page 328 – Figure 6-34 Cyclone Data Selected for Display; Cyclone; CYCLONE; To display the Cyclone legend, select the; Figure 6-35 Cyclone Legend
  • Page 329 – AIRBORNE COLOR WEATHER RADAR; SYSTEM DESCRIPTION; Radar features include:; PRINCIPLES OF PULSED AIRBORNE WEATHER RADAR
  • Page 330 – NEXRAD AND AIRBORNE WEATHER RADAR; Figure 6-36 Radar Beam from a 12 inch Antenna; Figure 6-37 Radar Beam in Relation to the Curvature of the Earth
  • Page 331 – RADAR SIGNAL ATTENUATION
  • Page 332 – RADAR SIGNAL REFLECTIVITY; Figure 6-38 Precipitation Type and Reflectivity
  • Page 333 – Figure 6-39 Angle of Incidence
  • Page 334 – SAFE OPERATING DISTANCE; MAXIMUM PERMISSIBLE EXPOSURE LEVEL (MPEL); Figure 6-40 MPEL Boundary; BASIC ANTENNA TILT SETUP
  • Page 335 – PRACTICAL APPLICATION USING THE BASIC TILT SETUP; Closely monitor anything that enters the display.; Figure 6-41 Vertical Change in Radar Beam per Nautical Mile
  • Page 336 – WEATHER MAPPING AND INTERPRETATION; WEATHER DISPLAY INTERPRETATION; and rates shown in the table.; 0 dBZ and greater; Table 6-3 Precipitation Intensity Levels; the turbulence is considered severe.
  • Page 337 – Figure 6-42 Cell Irregularities; Steep Gradient; Figure 6-43 The Blind Alley - Horizontal Scan
  • Page 338 – Figure 6-44 The Blind Alley; The Blind Alley at Close Range; may be present if the following characteristics are observed:
  • Page 339 – OPERATION IN WEATHER MODE; to Standby mode on landing.; Figure 6-45 Horizontal Scan Display; Radar Mode Scan Line
  • Page 340 – Figure 6-46 Confirming Activating Radar; YES
  • Page 341 – adjustment of the Bearing Line.; Figure 6-47 Bearing Line on Horizontal Scan; Bearing Line
  • Page 342 – Figure 6-48 Vertical Scan Display
  • Page 343 – Figure 6-49 Adjusting Tilt on Vertical Scan Display; Scan Line
  • Page 344 – GAIN; Calibrated Gain; Figure 6-50 Gain Calibration
  • Page 345 – Figure 6-51 Selecting Sector Scan Position
  • Page 346 – To activate or deactivate the antenna stabilization, select the; MODE; STAB ON; Softkey to activate antenna stabilization or select the; STAB OFF; Softkey to deactivate. The
  • Page 347 – To activate or deactivate the WATCHTM feature, select the; Figure 6-53 Horizontal Scan Without and With WATCHTM
  • Page 348 – unwanted weather alerts, deselect the; Figure 6-54 Weather Alert Indications; Weather Alerts; To activate or deactivate Weather Alerts, select the; Figure 6-55 Weather Alert on PFD
  • Page 349 – GROUND MAPPING AND INTERPRETATION; 7 dB and greater; Table 6-4 Ground Target Return Intensity Levels
  • Page 350 – Satellite Weather Lightning; Lightning Age; Strike is less than 6 seconds old; Table 6-5 Lightning Age and Symbols; SETTING UP STORMSCOPE ON THE NAVIGATION MAP
  • Page 351 – Figure 6-56 Page Menu
  • Page 352 – CELL AND STRIKE MODE ON THE NAVIGATION MAP; large FMS; Figure 6-58 Navigation Map Page with Stormscope
  • Page 353 – Manually clearing Stormscope data on the Navigation Map:; Figure 6-59 Navigation Map Page Options Menu; ZOOM RANGE ON THE NAVIGATION MAP; Figure 6-60 Lightning Display Range Annunciation; selected maximum zoom range is decluttered.
  • Page 354 – small; SELECTING THE STORMSCOPE PAGE; Figure 6-61 Stormscope Page
  • Page 355 – Figure 6-62 Navigation Map Page Options Menu
  • Page 356 – VIEW
  • Page 357 – TERRAIN PROXIMITY; intended only to enhance situational awareness.
  • Page 358 – DISPLAYING TERRAIN PROXIMITY DATA; Unlighted Obstacle; TERRAIN; Softkey to display terrain and obstacle data.
  • Page 359 – Figure 6-65 Navigation Map Page Setup Menu
  • Page 360 – panning feature is enabled by pressing the; Figure 6-67 Terrain Information on the Navigation Map Page; TERRAIN PROXIMITY PAGE; RANGE; Displaying the Terrain Proximity Page:; ARC
  • Page 361 – Figure 6-68 Terrain Proximity Page
  • Page 362 – situational awareness.
  • Page 363 – DISPLAYING TAWS DATA; Figure 6-70 Terrain Altitude/Color Correlation for TAWS; Table 6-7 TAWS Obstacle Colors and Symbology
  • Page 365 – Figure 6-72 Navigation Map Page Setup Menu; TAWS PAGE; from 1 to 200 nm, as indicated by the map range rings or arcs.
  • Page 366 – Showing/hiding aviation information on the TAWS Page:
  • Page 367 – TAWS ALERTS; • Press the; Figure 6-76 Alert Annunciation on the PFD; Alert Annunciation
  • Page 368 – Figure 6-78 TAWS PULL UP Alert Annunciation on the MFD; Alert; TAWS INHIBIT; Figure 6-79 TAWS Alerting Disabled (TAWS Inhibited) Annunciation; Select the TAWS Page.; INHIBIT; Softkey to inhibit TAWS.
  • Page 369 – Alert Type; configuration are indicated with asterisks.; Table 6-8 TAWS Alerts Summary
  • Page 370 – EXCESSIVE DESCENT RATE ALERT; Figure 6-80 Excessive Descent Rate Alert Criteria
  • Page 371 – FORWARD LOOKING TERRAIN AVOIDANCE; Flight Phase; Enroute
  • Page 372 – PREMATURE DESCENT ALERTING; the normal approach path to a runway.; PDA Alerting Area; Figure 6-81 PDA Alerting Threshold; FIVE-HUNDRED AURAL ALERT
  • Page 373 – NEGATIVE CLIMB RATE AFTER TAKEOFF ALERT (NCR); • Height above the terrain is less than 700 feet; “DON’T SINK”
  • Page 374 – SYSTEM STATUS; Table 6-10 TAWS System Test Status Annunciations; Manually testing the TAWS System:; Select Test TAWS and press the; Key to confirm the selection.; Figure 6-83 TAWS Page Menu
  • Page 375 – “TAWS Not Available”; Table 6-11 TAWS Status Annunciations
  • Page 376 – TIS is disabled when Traffic Advisory System (TAS) is installed.; Figure 6-84 TAS Traffic Softkeys; TAS SYMBOLOGY; TAS Symbol; Traffic Advisory Off Scale; Table 6-12 TAS Symbol Description; ±1200 feet relative altitude or the distance is beyond 5 nm.
  • Page 377 – OPERATION; The KTA 870 automatically transitions from; knob
  • Page 378 – Figure 6-85 Traffic Map Page; DISPLAYING TRAFFIC DATA; TRAFFIC; Softkey. Traffic is now displayed on the map.
  • Page 379 – Figure 6-86 TAS Traffic on Navigation Map; ALTITUDE DISPLAY; On the Traffic Page, select the
  • Page 380 – TRAFFIC MAP PAGE DISPLAY RANGE; from 2 to 40 nm, as indicated by the map range rings.
  • Page 381 – Key to select an option.; Knob or; Key to return to the Navigation Map Page.; Figure 6-88 Navigation Map Page Setup Menu
  • Page 382 – TAS ALERTS; remaining displayed until no TAs are detected in the area.; Inset Map; Mode; TAS Self-test Initiated; TEST; TAS Operating; OPERATING; TAS Standby; STANDBY; * See Table 6-14 for additional failure annunciations; Table 6-13 TAS Modes
  • Page 383 – Table 6-14 TAS Failure Annunciations; maps on which traffic can be displayed.; Data is not being received from the TAS unit; *Shown as symbol on Traffic Map Page; Table 6-15 TAS Traffic Status Annunciations
  • Page 385 – AUTOMATIC FLIGHT CONTROL SYSTEM
  • Page 386 – Annunciator Light; Figure 7-1 GMC 710 AFCS Control Unit
  • Page 388 – FLIGHT DIRECTOR OPERATION; ACTIVATING THE FLIGHT DIRECTOR; VNV
  • Page 389 – AFCS STATUS BOX; Figure 7-2 PFD AFCS Display
  • Page 390 – FLIGHT DIRECTOR MODES; Figure 7-3 Loss of VOR Signal; director modes becomes invalid or unavailable.; SWITCHING FLIGHT DIRECTORS; Figure 7-4 Flight Director Selection Indications; Pilot-side Flight Director
  • Page 391 – COMMAND BARS; Aircraft Symbol
  • Page 392 – Wheel are also listed in the table.; ALTS; instead of VNV Target Altitude; Table 7-2 Flight Director Vertical Modes
  • Page 393 – When the flight director is activated (the; CHANGING THE PITCH REFERENCE; • Using the; Figure 7-7 Pitch Hold Mode
  • Page 394 – Figure 7-8 Automatic Mode Transitions During Altitude Capture; Altitude Reference; CHANGING THE SELECTED ALTITUDE; CWS; ALT SEL
  • Page 395 – Altitude Hold Mode can be activated by pressing the; CHANGING THE ALTITUDE REFERENCE; Turning the; flight director’s Altitude Reference, and does not cancel the mode.; Figure 7-9 Altitude Hold Mode
  • Page 396 – VS; CHANGING THE VERTICAL SPEED REFERENCE; Button must be pressed again after the Selected; Figure 7-10 Vertical Speed Hold Mode
  • Page 397 – Flight Level Change Mode is selected by pressing the
  • Page 398 – CHANGING THE AIRSPEED REFERENCE
  • Page 399 – Section for more information on VNV flight plans.; When a vertical profile (VNV flight plan) is active and the; Figure 7-13 Vertical Path Tracking Armed Annunciations
  • Page 400 – • Pressing the; Figure 7-14 Vertical Path Capture
  • Page 401 – Figure 7-15 Vertical Path Tracking Mode
  • Page 402 – revert to Pitch Hold Mode:; Figure 7-16 Flight Level Change VNV Non-Path Descent
  • Page 403 – after the; Flash up to 10 sec, Indicating Automatic Transition; Figure 7-17 VNV Altitude Capture; VNV T
  • Page 404 – Figure 7-18 Glidepath Mode Armed; • The active waypoint is at or after the final approach fix (FAF).; Figure 7-19 Glidepath Mode
  • Page 405 – Figure 7-20 Glideslope Mode Armed
  • Page 406 – GA; Figure 7-22 Go Around Mode
  • Page 407 – of the Attitude Indicator.; Table 7-3 Flight Director Lateral Modes
  • Page 408 – Bank Angle; Rolls wings level; Table 7-4 Roll Hold Mode Responses; CHANGING THE ROLL REFERENCE; LOW BANK MODE; BANK; Figure 7-25 Low Bank Mode Limits; Low Bank Arc
  • Page 409 – Heading Select Mode is activated by pressing the; CHANGING THE SELECTED HEADING; HDG; Knob synchronizes the Selected Heading to the current heading.; Figure 7-26 Heading Select Mode
  • Page 410 – flight director to enter Navigation Mode.; Figure 7-27 GPS Navigation Mode Armed; APR
  • Page 411 – CHANGING THE SELECTED COURSE; Course is controlled using the; Figure 7-28 Navigation Mode
  • Page 412 – flight director to enter Approach Mode.; Figure 7-29 GPS Approach Mode Armed
  • Page 413 – CRS
  • Page 414 – BC; Figure 7-30 Backcourse Mode
  • Page 415 – AUTOPILOT AND YAW DAMPER OPERATION; FLIGHT CONTROL; PITCH AXIS AND TRIM; MEPT; ROLL AXIS
  • Page 416 – ENGAGEMENT; AP; Figure 7-31 Autopilot and Yaw Damper Engaged; YD; CONTROL WHEEL STEERING; Figure 7-32 CWS Annunciation
  • Page 417 – DISENGAGEMENT; Key does not disengage the yaw damper.; Figure 7-33 Manual Autopilot Disengagement
  • Page 418 – EXAMPLE FLIGHT PLAN; Figure 7-36 Flight Plan Overview
  • Page 419 – DEPARTURE
  • Page 420 – Figure 7-37 Departure
  • Page 421 – INTERCEPTING A VOR RADIAL; Intercepting a VOR radial:; Figure 7-38 Intercepting a VOR Radial
  • Page 422 – FLYING A FLIGHT PLAN/GPS COURSE; currently tracking inbound on Airway V4.; Flying a GPS flight plan:; Transition from VOR to GPS Navigation Mode:; Softkey until GPS is the selected navigation source.; Figure 7-39 Transition to GPS Flight Plan
  • Page 423 – DESCENT; Three methods are presented for descent:; Figure 7-40 FLC Descent
  • Page 424 – Figure 7-41 VPTH Descent
  • Page 425 – Non-path descent using Flight Level Change Mode:; Using the; ,400 feet) at which to level off between VNV flight plan altitudes.; FLC
  • Page 427 – APPROACH; Figure 7-43 ILS Approach to KCOS
  • Page 428 – Figure 7-44 LPV Approach to KCOS
  • Page 429 – GO AROUND/MISSED APPROACH; Flashes 5 sec
  • Page 431 – AFCS ANNUNCIATIONS AND ALERTS; AFCS STATUS ALERTS; Figure 7-46 AFCS Status Annunciation; AFCS Status; Table 7-5 AFCS Status Alerts
  • Page 432 – OVERSPEED PROTECTION; Airspeed; Figure 7-47 Overspeed Annunciation
  • Page 433 – ADDITIONAL FEATURES; SECTION 8 ADDITIONAL FEATURES; Additional features of the G1000 include the following:
  • Page 434 – Figure 8-1 SafeTaxi Depiction on the Navigation Map Page
  • Page 435 – Figure 8-2 Navigation Map PAGE MENU, Map Setup Option; SafeTaxi
  • Page 436 – SAFETAXI CYCLE NUMBER AND REVISION; SafeTaxi Database is Current
  • Page 437 – Figure 8-5 AUX – System Status Page, SafeTaxi Current Information; SafeTaxi Data; DBASE
  • Page 438 – Current Date is before Effective Date
  • Page 439 – CHARTVIEW SOFTKEYS
  • Page 440 – TERMINAL PROCEDURES CHARTS; Navigation Map Page OPTIONS Menu; Figure 8-8 Option Menus
  • Page 441 – UNABLE TO DISPLAY CHART is then displayed.; Figure 8-10 Unable To Display Chart Banner; When a chart is not available by selecting the
  • Page 442 – Figure 8-11 Approach Information Page, Chart Selection; While the APPROACH Box is selected using the
  • Page 443 – Figure 8-12 CHRT Softkey, Airport Information Page; Select; CHRT
  • Page 444 – Selecting the; Aircraft; Figure 8-13 Airport Information Page, INFO View, Full Screen Width
  • Page 445 – Chart Not; Figure 8-15 Departure Information Page
  • Page 446 – Figure 8-16 Arrival Information Page; Figure 8-17 Approach Information Page
  • Page 447 – Figure 8-18 Weather Information Page; WX Softkey
  • Page 448 – A subdued softkey label indicates the function is disabled.; Figure 8-19 NOTAM Softkey Highlighted
  • Page 449 – Figure 8-20 Airport Information Page, Local NOTAMs; Local; NOTAM
  • Page 450 – CHART OPTIONS; Entire Chart; Figure 8-21 Approach Information Page, ALL View
  • Page 451 – Figure 8-22 Approach Information Page, Header View; Figure 8-23 Approach Information Page, Plan View
  • Page 453 – FIT WIDTH; FIT WDTH; Softkey to Show; Figure 8-26 Airport Information Page, FIT WDTH Softkey Selected
  • Page 454 – Figure 8-27 Airport Information Page, Full Screen and Info Window
  • Page 455 – Figure 8-28 Page Menus; Full Screen On/Off Selection
  • Page 456 – Figure 8-29 Waypoint Information Page, OPTIONS Menu
  • Page 457 – Figure 8-30 Arrival Information Page, Day View
  • Page 458 – CHARTVIEW CYCLE NUMBER AND EXPIRATION DATE; Power-up Page Display; Table 8-1 ChartView Power-up Page Annunciations and Definitions
  • Page 460 – ChartView; Appendix B for instructions on revising the ChartView database.
  • Page 462 – FLITECHARTS SOFTKEYS
  • Page 463 – Figure 8-36 Option Menus
  • Page 464 – Figure 8-38 Unable To Display Chart Banner
  • Page 465 – Figure 8-39 Approach Information Page, Chart Selection
  • Page 466 – Figure 8-40 CHRT Softkey, Airport Information Page
  • Page 467 – Info Box
  • Page 468 – Figure 8-43 Departure Information Page
  • Page 469 – Figure 8-44 Arrival Information Page; Figure 8-45 Approach Information Page
  • Page 470 – WX
  • Page 471 – Figure 8-47 Airport Information Page, ALL View Selected
  • Page 472 – Figure 8-48 Approach Information Page, FIT WDTH Softkey Selected
  • Page 473 – Figure 8-49 Airport Information Page, Full Screen and Info Window; FULL SCN; Softkey to Switch
  • Page 474 – Figure 8-50 Page Menus
  • Page 475 – Figure 8-51 Waypoint Information Page, OPTIONS Menu
  • Page 476 – Figure 8-52 Approach Information Page, Day View
  • Page 477 – FLITECHARTS CYCLE NUMBER AND EXPIRATION DATE; Table 8-2 FliteCharts Power-up Page Annunciations and Definitions
  • Page 478 – Figure 8-54 FliteCharts Power-up Page Messages
  • Page 479 – instructions on revising the FliteCharts database.
  • Page 480 – FliteCharts Disabled, FliteCharts Not Available
  • Page 481 – ACTIVATING XM SATELLITE RADIO SERVICES; These IDs are located:
  • Page 482 – RADIO
  • Page 483 – USING XM RADIO; Selecting the XM Radio Page:; Knob to select the Auxiliary Page Group.; Knob to select the displayed AUX - XM Information Page.; Figure 8-58 XM Radio Page
  • Page 484 – ACTIVE CHANNEL AND CHANNEL LIST
  • Page 485 – CATEGORY; Figure 8-59 Categories List
  • Page 486 – PRESETS; Figure 8-60 Accessing and Selecting XM Preset Channels; VOL; Figure 8-61 Volume Control
  • Page 487 – highlight the first empty scheduler message naming field.
  • Page 488 – highlight the name field of the scheduler message to be deleted.; Figure 8-63 PFD Alerts Window
  • Page 489 – Figure 8-64 Checklist Softkeys; CHKLIST
  • Page 490 – Figure 8-65 Checklist Page Example
  • Page 491 – Figure 8-66 Sample Checklist
  • Page 492 – ABNORMAL OPERATION; GDL 69/69A DATA LINK RECEIVER TROUBLESHOOTING; • Ensure the XM subscription has been activated; Selecting the System Status Page:; Knob to select the AUX Page Group.; Figure 8-67 LRU Information Window on System Status Page
  • Page 493 – Message; Table 8-3 GDL 69/69A Data Link Receiver Error Messages
  • Page 495 – APPENDIX A; ANNUNCIATIONS AND ALERTS; CAS MESSAGES; Warning Messages
  • Page 496 – Caution Messages
  • Page 497 – COMPARATOR ANNUNCIATIONS; Figure A-1 Sensor Comparator Window; Comparator; Comparator Window Text; ALT MISCOMP
  • Page 498 – REVERSIONARY SENSOR ANNUNCIATIONS; SENSOR; Figure A-2 Reversionary Sensor Windows; Reversionary; Reversionary Sensor; When a new message is issued, the; Softkey flashes if the state of a displayed message changes
  • Page 499 – Figure A-4 G1000 System Failure Annunciations
  • Page 500 – System Annunciation; Attitude and Heading Reference System is aligning.
  • Page 501 – G1000 SYSTEM MESSAGE ADVISORIES; MFD & PFD MESSAGE ADVISORIES
  • Page 502 – DATABASE MESSAGE ADVISORIES
  • Page 505 – GMA 1347D MESSAGE ADVISORIES
  • Page 507 – GEA 71 MESSAGE ADVISORIES
  • Page 508 – GTX 33 & GTX 33D MESSAGE ADVISORIES
  • Page 509 – GMU 44 MESSAGE ADVISORIES
  • Page 510 – GDC 74B MESSAGE ADVISORIES
  • Page 511 – MISCELLANEOUS MESSAGE ADVISORIES
  • Page 513 – AFCS ALERTS; Figure A-5 AFCS System Status Field; System Status Field; Do not press the; AP DISC
  • Page 515 – TAWS SYSTEM STATUS ANNUNCIATIONS
  • Page 517 – APPENDIX B; SD CARD USE; JEPPESEN DATABASES; be used to update the PFD and the MFD.; Updating the Jeppesen aviation database:; Figure B-1 Database Update Prompt; Figure B-2 Database Update Confirmation
  • Page 518 – After the update completes, the PFD starts in normal mode.; GARMIN DATABASES; Figure B-3 Correct Database Locations; MFD
  • Page 519 – UPDATING GARMIN DATABASES; • Windows-compatible PC computer (Windows 2000 or XP recommended)
  • Page 520 – Figure B-4 Database Information on the Splash Screen
  • Page 521 – APPENDIX C; GLOSSARY
  • Page 527 – APPENDIX D; FREQUENTLY ASKED QUESTIONS; WAAS; performs the following functions:
  • Page 528 – OBS S
  • Page 531 – after
  • Page 533 – APPENDIX E; AIRPORT; NAVAIDS; Item; LINE SYMBOLS; Item; Section for XM Weather Product legends.
  • Page 534 – MISCELLANEOUS; STORMSCOPE LIGHTNING STRIKES
  • Page 535 – TERRAIN AVOIDANCE COLORS AND SYMBOLS; Figure E-1 Terrain Proximity Color Chart; Terrain more than 1000 ft below the aircraft altitude; Figure E-2 TAWS Color Chart; Obstacle Symbol; Red; Obstacle Symbols and Colors
  • Page 536 – HAZARD AVOIDANCE FEATURES; This table identifies the symbols displayed in the; Feature
  • Page 540 – Nearest
  • Page 541 – Terrain Awareness and Warning System (TAWS)
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Socata

TBM 850

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Summary

Page 2 - Garmin G1000 Pilot’s Guide for the Socata TBM 850

Garmin G1000 Pilot’s Guide for the Socata TBM 850 190-00709-00 Rev. A 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 compar...

Page 3 - LIMITED WARRANTY

190-00709-00 Rev. A Garmin G1000 Pilot’s Guide for the Socata TBM 850 i LIMITED WARRANTY LIMITED WARRANTY This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this period, Garmin will, at its sole option, repair or repla...

Page 4 - ii; WARNING; Aeronautical; Information

Garmin G1000 Pilot’s Guide for the Socata TBM 850 190-00709-00 Rev. A ii WARNINGS, CAUTIONS, AND 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 ter...

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