Garmin Flight Deck 100 - Manual

Garmin Flight Deck 100

Garmin Flight Deck 100 – Manual, read for free online in PDF format. We hope this helps you resolve any issues you may have. If you have further questions, please contact us through the contact form.

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Table of Contents:

  • Page 4 – ii; LIMITED WARRANTY
  • Page 5 – iii
  • Page 6 – iv; Aeronautical; Information
  • Page 7 – NOTE
  • Page 8 – REVISION INFORMATION
  • Page 9 – vii; TABLE OF CONTENTS; SECTION 1 SYSTEM OVERVIEW
  • Page 10 – viii; SECTION 5 FLIGHT MANAGEMENT
  • Page 11 – ix; SECTION 6 HAZARD AVOIDANCE
  • Page 12 – SECTION 8 ADDITIONAL FEATURES
  • Page 13 – SYSTEM OVERVIEW; SYSTEM DESCRIPTION; Refer to the AFCS section for details on the GFC 700 AFCS.
  • Page 14 – DISPLAY BACKUP; button) and communicates with the on-side
  • Page 15 – with both GIA 63Ws using an RS-485 digital interface.
  • Page 16 – an RS-232 digital interface. These transponders
  • Page 17 – Communication is through the High Speed Data Bus.
  • Page 19 – Figure 1-1 System LRU Configuration
  • Page 20 – CONTROLS; and AFCS sections respectively.; Figure 1-2 PFD Controls
  • Page 22 – MFD CONTROL UNIT
  • Page 23 – AFCS CONTROLS
  • Page 24 – (Manual Electric Pitch Trim) Switch are additional AFCS
  • Page 25 – AUDIO PANEL CONTROLS; COM1 MIC; – When selected, audio from the #1 Com receiver can be heard.; COM2 MIC; Key, or COM1 can be added by pressing the
  • Page 26 – Press during play to play the previously recorded memory; PLAY; Key will begin playing the next previously recorded block.
  • Page 27 – SOFTKEY FUNCTION; Softkey On; Selecting a softkey using the MFD Control Unit; Press the center of the; SEL; Key to select the desired softkey.; PFD SOFTKEYS
  • Page 32 – Figure 1-7 Top Level PFD Softkeys; Figure 1-9 INSET Map Softkeys; Figure 1-10 SENSOR Softkeys
  • Page 33 – Figure 1-11 PFD Configuration Softkeys
  • Page 34 – MFD SOFTKEYS; Accesses EIS softkeys
  • Page 36 – Figure 1-14 Top Level MFD Softkeys
  • Page 37 – SECURE DIGITAL CARDS; Refer to the Appendices for instructions on updating databases.; tall an SD card; Rem; ove an SD card; Figure 1-17 Display Bezel SD Card Slots
  • Page 38 – and emergency power supply operation.; ENT; Key; Figure 1-18 PFD Initialization
  • Page 39 – SYSTEM OPERATION; In the event of display failure, the display modes are as follows:; PFD1 failure; – MFD enters reversionary mode PFD2 remains in normal mode.; MFD failure; – PFD1 and PFD2 enter reversionary mode.; PFD2 failure; – PFD1 and the MFD remain in normal mode.; NORMAL OPERATION; PFD; Figure 1-20 gives an example of the system displays in normal mode.; Figure 1-20 Normal Operation
  • Page 40 – REVERSIONARY MODE; further information regarding system-specific alerts.; Figure 1-21 Reversionary Mode; Figure 1-22 DISPLAY BACKUP Button
  • Page 41 – AHRS OPERATION; Refer to the Appendices for specific AHRS alert information.; Air Data; Figure 1-23 AHRS Operation
  • Page 42 – PRODIGY
  • Page 43 – Figure 1-24 System Failure Annunciations; GPS RECEIVER OPERATION
  • Page 44 – Or
  • Page 45 – RAIM
  • Page 47 – • ‘COMPUTING AVAILABILITY’—RAIM calculation in progress; SBAS; , and turn the large FMS Knob to highlight the desired SBAS system.
  • Page 48 – ACCESSING SYSTEM FUNCTIONALITY; MENUS; Figure 1-26 Page Menu Examples; No Options with NRST; MFD PAGE GROUPS; FMS; Knob. The page group tabs
  • Page 49 – Figure 1-27 Page Title and Page Groups; The main page groups are navigated using the; Knob specific pages within each group can vary depending; Selecting a page using the; large; Turn; Knob, then with the appropriate softkey at the bottom of the page
  • Page 50 – Figure 1-28 Map Pages; optional; Figure 1-29 Waypoint Pages; Airport; DP
  • Page 51 – Figure 1-30 Auxiliary Pages
  • Page 52 – Figure 1-31 Flight Plan Pages; VIEW; Figure 1-32 System Pages; CHKLIST
  • Page 53 – Figure 1-33 Nearest Pages; PROC; Figure 1-34 Procedure Pages; Procedure Pages
  • Page 54 – MFD SYSTEM PAGES; SYSTEM SETUP PAGE; Figure 1-35 System Setup Page
  • Page 55 – Knob to highlight ‘CREATE’ in the Pilot Profile Box.
  • Page 56 – Knob to highlight ‘RENAME’ in the Pilot Profile Box.; another profile, then delete the desired profile.
  • Page 57 – Pilot Profile Importing and Import
  • Page 58 – Pilot Profile Exporting Window, Enter a
  • Page 59 – Knob to highlight the time format field in the Date/Time Box.; Affects the BRG field in the PFD Navigation Status Box.; Baro t
  • Page 60 – • Class D; S Knob to select the ON/OFF field in the Arrival Alert Box.
  • Page 61 – Knob to highlight the distance field in the Arrival Alert Box.; Knob; mfD D
  • Page 62 – The GPS CDI Box on the System Setup Page displays the following:
  • Page 63 – COM frequency channel spacing.; Indicators and the altimeter barometric settings.
  • Page 64 – Figure 1-39 System Status Page
  • Page 65 – Figure 1-40 Utility Page
  • Page 66 – aircraft lifts off the timer can also be reset to zero at any time.
  • Page 67 – MENU
  • Page 68 – highlight the name field of the scheduler message to be deleted.; Softkey opens the; Softkey is pressed again, the; Figure 1-41 PFD Message Window
  • Page 69 – DISPLAY BACKLIGHTING; AUTOMATIC ADJUSTMENT; also be adjusted from the MFD.; Adjust display backlighting manually:; Figure 1-42 Manual Display Backlighting Adjustment
  • Page 70 – Adjust key backlighting manually:; Figure 1-43 Manual Key Lighting Adjustment
  • Page 71 – FLIGHT INSTRUMENTS; SECTION 2 FLIGHT INSTRUMENTS
  • Page 73 – Figure 2-2 Additional PFD Information
  • Page 74 – FLIGHT INSTRUMENTS; AIRSPEED INDICATOR; Figure 2-3 Airspeed Indicator; . An open green circle on the airspeed tape represents 1.3V
  • Page 75 – Vspeed; FS; RF; AC; FS; Table 2-1 Vspeed Flag Labels
  • Page 76 – a category of Vspeeds can also be restored.
  • Page 77 – ATTITUDE INDICATOR; Figure 2-6 Attitude Indicator; of the pointer on the roll scale.
  • Page 78 – Figure 2-8 Flight Director Format
  • Page 79 – ALTIMETER; The; Setting the Selected Altitude:; Turn the; ALT SEL; Altitude is adjusted in 50 meter increments.
  • Page 80 – Figure 2-10 Altimeter Setting in hPa and Altitude in Meters
  • Page 81 – Figure 2-11 Standard Barometric Altimeter Setting; Barometric Settings
  • Page 82 – through this altitude and the; STD BARO; BARO, the setting flashes in light blue until it is changed.; Figure 2-13 Baro Transition Alert
  • Page 83 – VERTICAL DEVIATION; Figure 2-14 Vertical Speed and Vertical Deviation Indications
  • Page 85 – Selected Course is shown to the upper; Figure 2-17 Heading and Course Indications
  • Page 86 – Figure 2-19 System Setup Page, Navigation Angle Settings
  • Page 87 – Figure 2-20 Turn Rate Indicator and Trend Vector; BEARING POINTERS AND INFORMATION WINDOWS; Two; Figure 2-21 HSI with Bearing and DME Information
  • Page 88 – • GPS-derived great circle distance to; DME INFORMATION WINDOWS
  • Page 89 – Figure 2-22 Course Deviation Indicator
  • Page 90 – CDI; Figure 2-24 Selecting a Navigation Source; when all of the following occur:
  • Page 91 – Figure 2-25 System Setup Page, CDI Synchronization
  • Page 92 – Figure 2-26 System Setup Page, GPS CDI Setting
  • Page 93 – Figure 2-27 Automatic CDI Scaling; phase of flight is automatically entered and CDI scaling
  • Page 94 – Figure 2-28 Typical LNAV and LNAV+V Approach CDI Scaling; • When a; conditions exist the color changes to yellow.; Table 2-2 Automatic GPS CDI Scaling
  • Page 95 – OBS
  • Page 96 – Figure 2-31 Suspending Automatic Waypoint Sequencing; Softkey
  • Page 97 – SUPPLEMENTAL FLIGHT DATA; Selecting the; DFLTS; TEMPERATURE DISPLAYS; The Total and; Figure 2-32 Total and Static Air Temperatures; Normal
  • Page 98 – WIND DATA; Figure 2-33 Wind Data; Option 2
  • Page 99 – Aircraft > 1 min before the next TOD due to flight plan change; Table 2-3 VNV Indication Removal Criteria
  • Page 100 – PFD ANNUNCIATIONS AND ALERTING FUNCTIONS; Softkey flashes to alert the flight crew. It continues to flash; Figure 2-35 Prodigy Alerting System
  • Page 101 – MARKER BEACON ANNUNCIATIONS; Figure 2-36 Marker Beacon Annunciations; TRAFFIC ANNUNCIATIONS; Traffic
  • Page 102 – TAWS ANNUNCIATIONS; Figure 2-38 Example TAWS-A Annunciations; ALTITUDE ALERTING; The following occur when approaching the Selected Altitude:; Figure 2-39 Altitude Alerting Visual Annunciations; Deviation of ±200 feet
  • Page 103 – LOW ALTITUDE ANNUNCIATION; inhibited in order for this annunciation to be shown.; Figure 2-40 Low Altitude on GPS SBAS Approach; MINIMUM DESCENT ALTITUDE/DECISION HEIGHT ALERTING
  • Page 105 – RADAR ALTIMETER; Figure 2-43 Current Radar Height; Radar Altimeter; Radar Height Range; Table 2-4 Radar Altimeter Sensitivity
  • Page 106 – Figure 2-47 Radar Altimeter Invalid Data
  • Page 107 – ABNORMAL OPERATIONS; Annunciation; LOI; Table 2-5 Abnormal GPS Conditions Annunciated on HSI; the following items on the PFD to be shown in yellow:
  • Page 108 – UNUSUAL ATTITUDES; Figure 2-49 Pitch Attitude Warnings; Nose High
  • Page 109 – ENGINE & AIRFRAME SYSTEMS; SECTION 3 ENGINE AND AIRFRAME SYSTEMS; The Prodigy; Engine Indication System; information on the left side of the Multi Function Display (MFD).; Synoptics pages; • The; Crew Alerting System
  • Page 110 – EIS
  • Page 111 – FMS LFE; * Softkey disabled while aircraft is on the ground
  • Page 113 – TAKEOFF DATA SET WINDOW; Figure 3-6 Takeoff Data Set Window; ATR enabled in both engines; ATR; ATR armed in both engines, but inactive; * When no indication is shown, ATR has not been
  • Page 114 – ENGINE INDICATIONS; Figure 3-7 Engine and Oil Indications
  • Page 115 – On the N1 gauges, the following indications can be displayed:; Figure 3-8 Engine Shutdown Indication; THRUST RATING; Indication; Cruise; CLB; Climb; CON; Continuous; TO; Takeoff; GA; Go Around; Table 3-2 Thrust Rating Indications
  • Page 116 – reached for the corresponding engine.; Figure 3-9 N1 Current Speed Control Limit; CSC; FUEL AND ELECTRICAL INDICATIONS; Figure 3-10 Fuel Display; Total Fuel Quantity; Figure 3-11 Electrical Display
  • Page 117 – CABIN PRESSURIZATION; Figure 3-12 Cabin Display
  • Page 118 – SPOILER AND LANDING GEAR; Figure 3-13 Spoiler and; Table 3-3 Spoiler Indications; Table 3-4 Landing Gear Position Indications; FLAPS AND TRIM; Figure 3-14 Flap and Trim Indications
  • Page 119 – SYSTEM STATUS; Figure 3-15 System Status Synoptics Page
  • Page 120 – Figure 3-16 Environmental Control System Synoptics Page
  • Page 121 – Unit; Fan; Table 3-5 Environmental Control System Unit Status Indications
  • Page 122 – ELECTRICAL; Bus; Figure 3-17 Electrical Synoptics Page; Ground Power Unit; Generator; Table 3-6 Electrical System Unit Status Indications
  • Page 123 – FUEL; indicates invalid data or a failed unit.; Figure 3-18 Fuel Synoptics Page; Fuel Line; Table 3-7 Fuel System Unit Status Indications
  • Page 124 – ICE PROTECTION SYSTEM; Figure 3-19 Ice Protection Synoptics Page
  • Page 125 – Open with flow; Table 3-8 Ice Protection System Unit Status Indications
  • Page 126 – ENGINE MAINTENANCE; Refer to the Airplane Flight Manual (AFM) for required actions.; CLEAR E1; and; CLEAR E2; Figure 3-20 Engine Maintenance Synoptics Page
  • Page 127 – CAS; CAS MESSAGE PRIORITIZATION; flashing ‘ADVISORY’ softkey.
  • Page 128 – CAS MESSAGES; WARNING MESSAGES; Message; ELEC EMERGENCY; Table 3-9 Warning CAS Messages
  • Page 129 – A leakage has been detected at the bleed 1 line.
  • Page 130 – GIA 1 FAIL
  • Page 131 – SWPS UNTESTED; ADVISORY MESSAGES; DC BUS 1 OFF
  • Page 132 – EMER BUS OFF; Limit exceeded in engine(s) during flight; GEA 1 FAIL; Table 3-11 Advisory CAS Messages
  • Page 133 – ABNORMAL OPERATIONS; ENGINE; Figure 3-23 Engine Failure Indication; background, and the trend arrow turns red.; Figure 3-25 Cabin Display with Excessive Change Rate
  • Page 134 – FLAPS; The following denote abnormal flap conditions:; TRIM; Rudder
  • Page 135 – AUDIO PANEL AND CNS; SECTION 4 AUDIO PANEL AND CNS; or TCAS II Mode S Transponder; Knob located on the PFD. The; AUDIO PANEL VOLUME CONTROL
  • Page 136 – MFD/PFD CONTROLS AND FREQUENCY DISPLAY
  • Page 137 – – Transfers the standby and active NAV frequencies.
  • Page 138 – Figure 4-2 Audio Panel Controls; added by pressing the; COM3 MIC
  • Page 140 – COM TRANSCEIVER SELECTION AND ACTIVATION; COM transceiver state prior to shutdown.; COM MIC; Keys on the Audio Panel.; or; Key is selected on the Audio Panel, both active COM; Figure 4-3 Selecting a COM Radio for Transmit
  • Page 141 – During COM transmission, a white; Key Annunciator flashes approximately once per second.; 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 142 – Press the small; upper and lower radio frequency fields.; Figure 4-6 Switching COM Tuning Boxes; COM; Knob to; Pressing and holding the COM; Key for two seconds automatically loads the emergency; Key activates the transceiver.; Press for Two Seconds to
  • Page 143 – AUTO-TUNING THE COM FREQUENCY; COM frequencies can be automatically tuned from the following:; AUTO-TUNING FROM THE PFD; the PFD. When the desired frequency is entered, it becomes a; Frequency; Key places this frequency into the COM Active Frequency Field.; Select the; NRST; Softkey to Open
  • Page 144 – page group by highlighting the frequency and pressing the; Figure 4-9 Frequency Auto-Tuning from the MFD; Figure 4-10 Nearest Pages Menus
  • Page 145 – Figure 4-11 WPT – Airport Information Page
  • Page 147 – FREQUENCY SPACING; Figure 4-13 COM Channel Spacing; Spacing; While the COM CONFIG Box is selected, the softkeys are blank.; Figure 4-14 AUX – System Setup Page; COM Frequency
  • Page 148 – 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 149 – NAV RADIO SELECTION AND ACTIVATION; A NAV radio is selected for navigation by selecting the; Figure 4-17 Selecting a NAV Radio for Navigation
  • Page 150 – ADF; optional DME 1 audio; AUX; optional DME 2 audio.; 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 151 – Figure 4-20 Switching NAV Tuning Boxes; Knob turns off the Morse code audio only in the radio with the NAV; Figure 4-21 NAV Radio ID Indication; NAV Radio volume level can be adjusted from 0 to 100% using the; Figure 4-22 NAV Volume Levels
  • Page 152 – AUTO-TUNING A NAV FREQUENCY FROM THE MFD; • WPT – Airport Information; Figure 4-23 NAV Frequency Auto-Tuning from the MFD
  • Page 153 – Figure 4-24 Nearest Pages Menus; Nearest Airspaces Menu
  • Page 154 – In the example shown, the VOR list is selected with the; VOR; Softkey or from the page menu. The; Softkey and; FREQ
  • Page 155 – a similar manner using the appropriate softkeys or; NRST – Nearest Airports Pages
  • Page 156 – to a NAV frequency field as follows:
  • Page 157 – MARKER BEACON RECEIVER; annunciations located to the left of the Altimeter on the PFD.; Figure 4-27 Marker Beacon Annunciations on the PFD; Pressing the; HI SENS
  • Page 158 – DME; Active and; Knob activates/deactivates the selection cursor; Knob and the
  • Page 159 – the previously entered frequency.; CLR
  • Page 160 – Selecting an ADF receiver mode:; Turn the large; Knob to place the selection cursor over the ADF mode field.; Knob to select the desired ADF receiver mode.; Figure 4-32 Selecting ADF Receiver Mode; Turn the Small
  • Page 161 – and the NAV1; Figure 4-33 DME Tuning Window; The following DME transceiver pairings can be selected:; Selecting DME transceiver pairing:; Key or; Knob while in the process of; Knob activates/deactivates the cursor in
  • Page 162 – MODE S TRANSPONDER
  • Page 163 – GTX 33/33D TRANSPONDER CONTROLS; the transponder code. If an error is made, selecting the; Selecting and activating Transponder 1 or Transponder 2:; XPDR; Softkey to display the Transponder Mode Selection Softkeys.
  • Page 164 – GTX 33/33D TRANSPONDER MODE SELECTION; Selecting a transponder mode:; Code Number and; Figure 4-35 Standby Mode; ON Mode
  • Page 165 – selected manually by selecting the; ALT; Softkey. ALT Mode generates Mode A and Mode C replies. Acquisition; ALT Mode; Figure 4-37 Altitude Mode; GROUND MODE; the Transponder Data Box. In; GND; Figure 4-38 Ground Mode; REPLY STATUS; reply status field of the Transponder Data Box.; Reply to; Figure 4-39 Reply Indication
  • Page 166 – Selection, and Mode Selection or Code Entry. When the top-level
  • Page 167 – TCAS II TRANSPONDER MODE SELECTION (OPTIONAL); Figure 4-41 Standby Mode
  • Page 168 – operation in On Mode.; ON; Softkey. ON Mode generates Mode A replies,; Figure 4-43 Altitude Mode
  • Page 169 – ENTERING A TRANSPONDER CODE; Figure 4-44 Entering a Code; Key or small; Figure 4-45 Entering a Code with the FMS Knob
  • Page 170 – VFR code can be entered either manually or by selecting the; Figure 4-46 VFR Code; IDENT FUNCTION; In Standby Mode, the; Softkey is inoperative.; IDENT
  • Page 171 – FLIGHT ID REPORTING; center for configuration.; Key returns to the original Flight ID entry. While; using the same procedure.; Flight ID
  • Page 172 – ADDITIONAL AUDIO PANEL FUNCTIONS; SPEAKER; Key selects and deselects the on-side; SPKR; the side in which the oxygen mask is in use.; Figure 4-49 Music and Speaker Keys
  • Page 173 – INTERCOM; • When the MAN SQ Annunciator is illuminated (Manual Squelch), the; Figure 4-50 Intercom Controls
  • Page 174 – A passenger address system is provided by pressing the; Figure 4-51 PA Key Selected for Cabin Announcements; PA Key is Selected on; SIMULTANEOUS COM OPERATION
  • Page 175 – CLEARANCE RECORDER AND PLAYER; Key within one-half second backtracks through the; Figure 4-52 Play Key
  • Page 176 – ENTERTAINMENT INPUTS; can be adjusted by a Garmin-authorized service center.; MUSIC 1; MUSIC 1 can be heard by the pilot and copilot when the; mUsic 1 m; MUSIC
  • Page 177 – AUDIO PANELS PREFLIGHT PROCEDURE; When the; MAN SQ; Figure 4-53 Audio Panel Controls
  • Page 178 – Figure 4-54 Radio and Headphone Volume Controls
  • Page 179 – ABNORMAL OPERATION; equipment, including switches and external devices.; STUCK MICROPHONE; Figure 4-55 Stuck Microphone Alert; COM TUNING FAILURE; Figure 4-56 COM Tuning Failure; Emergency Channel
  • Page 180 – PFD FAILURE, DUAL SYSTEM; automatically tunes 121.500 MHz, but the frequency is not shown.; Figure 4-57 Frequency Section of PFD2 Display after PFD1 Failure
  • Page 181 – AUDIO PANEL FAIL-SAFE OPERATION; The red; Button selects the; Figure 4-59 Reversionary Mode Button
  • Page 183 – FLIGHT MANAGEMENT; Softkey. Pressing the; INSET; Softkey again, then pressing the; OFF; Softkey removes the Inset Map.; DCLTR
  • Page 184 – Figure 5-1 GPS Navigation Information on the PFD; NAVIGATION STATUS BOX; PFD Navigation Status Box
  • Page 185 – right to 021 ̊ in 8 seconds’); The symbols used in the PFD status bar are:; MFD Navigation Status Box
  • Page 186 – USING MAP DISPLAYS; Wind direction and speed; MAP ORIENTATION; Figure 5-3 Map Orientation
  • Page 187 – show the map orientation nor the wind direction and speed.; Figure 5-4 Navigation Map Page Menu Window; Map Setup; Figure 5-5 Map Setup Menu Window - Map Group; Orientation Field
  • Page 188 – MAP RANGE; Joystick; Figure 5-6 Map Range
  • Page 190 – Manual Range Override
  • Page 191 – MAP PANNING; Map panning allows the pilot to:; , the Map Pointer flashes on the map display.; Figure 5-8 Navigation Map - Map Pointer Activated; Map Pointer
  • Page 192 – Figure 5-9 Navigation Map - Map Pointer on Point of Interest
  • Page 193 – Figure 5-10 Navigation Map - Map Pointer on Airspace; to display the Map Pointer.; to move the Map Pointer around the map.
  • Page 194 – Place the Map Pointer on a waypoint.; NAVAID
  • Page 195 – Airspace
  • Page 196 – MEASURING BEARING AND DISTANCE; Figure 5-13 Navigation Map - Measuring Bearing and Distance; Pointer
  • Page 197 – TOPOGRAPHY; TOPO Off; TOPO On; TOPO
  • Page 198 – Figure 5-15 Navigation Map Setup Menu - TOPO DATA Setup; TOPO DATA
  • Page 199 – Figure 5-17 Navigation Map Setup Menu - TOPO SCALE Setup
  • Page 200 – MAP SYMBOLS; Softkey is also discussed.; LAND SYMBOLS; The following items are configured on the land menu:; Off; Table 5-1 Land Symbol Information
  • Page 201 – The following items are configured on the aviation menu:; Active Flight Plan Waypoint (ACTIVE FPL WPT); Table 5-2 Aviation Symbol Information
  • Page 202 – Figure 5-18 Navigation Map Setup Menu - LAND DATA Setup; LAND DATA
  • Page 203 – Figure 5-19 Navigation Map Setup Menu - LAND GROUP Setup; Figure 5-20 Navigation Map Setup Menu - AVIATION GROUP Setup; Maximum Display Range
  • Page 204 – The declutter level is displayed in the; Softkey and next to the Declutter Menu Option.; Figure 5-21 Navigation Map - Declutter Level Indications; Declutter Level; Navigation Map Page Menu
  • Page 205 – various levels of declutter.; Table 5-3 Navigation Map Items Displayed by Declutter Level
  • Page 206 – AIRWAYS; Figure 5-22 Airways on MFD Navigation Page; Low Altitude
  • Page 207 – Key from the Navigation Map Page. The Airway range can also be; Figure 5-23 Navigation Map Setup Menu - AIRWAYS Setup; Airway Display Selection
  • Page 208 – 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 209 – WIND VECTOR; Figure 5-26 Navigation Map - Wind Vector; Wind Direction
  • Page 210 – NAV RANGE RING; Figure 5-27 Navigation Map - Nav Range Ring; Nav Range Ring
  • Page 211 – FUEL RANGE RING; Figure 5-28 Navigation Map - Fuel Range Ring; Range to Reserve Fuel
  • Page 212 – Figure 5-29 Navigation Map - Field of View; Lateral Field
  • Page 213 – SELECTED ALTITUDE INTERCEPT ARC; Figure 5-30 Navigation Map - Range to Altitude Arc; Range to; Press the FMS Knob to return to the Navigation Map Page.
  • Page 214 – used for all phases of flight planning and navigation.; Figure 5-31 Waypoint Information Window; to turn the small; Waypoints Window is displayed when the
  • Page 215 – Figure 5-32 Waypoint Information Window - Duplicate Identifier; AIRPORTS
  • Page 216 – Figure 5-33 Airport Information Page; Frequency, Phone Number
  • Page 217 – Figure 5-34 Airport Directory Page Example; Airport Information
  • Page 218 – Communication Frequencies; * May include Additional Information; Table 5-5 Airport Frequency Abbreviations; The system provides a; Softkey on the PFD, which gives the pilot quick access to; Figure 5-35 Nearest Airports Window on PFD
  • Page 219 – presses of the; Figure 5-36 Airport Information Window on PFD
  • Page 220 – Figure 5-37 Nearest Airport Page; LD APR
  • Page 221 – Figure 5-38 System Setup Page - Nearest Airport Selection Criteria; Nearest Airport Criteria
  • Page 222 – INTERSECTIONS; used to define the intersection.; Figure 5-39 Intersection Information Page
  • Page 223 – three boxes labeled ‘NEAREST INT’, ‘INFORMATION’, and ‘REFERENCE VOR’.; Figure 5-40 Nearest Intersections Page
  • Page 224 – NDB; Figure 5-41 NDB Information Page
  • Page 225 – Figure 5-42 Nearest NDB Page
  • Page 226 – Figure 5-43 VOR Information Page
  • Page 227 – Figure 5-44 Nearest VOR Page
  • Page 228 – USER WAYPOINTS; map using the; Figure 5-45 User Waypoint Information Page
  • Page 229 – Figure 5-46 Nearest User Waypoint Page; CREATING USER WAYPOINTS
  • Page 230 – Figure 5-47 User Waypoint Information Page Menu
  • Page 231 – the; EDITING USER WAYPOINTS
  • Page 234 – Figure 5-48 Airspaces; Restricted Area
  • Page 236 – Figure 5-49 System Setup Page - Airspace Alerts
  • Page 237 – Figure 5-50 Nearest Airspaces Page; Airspace Alerts Info; Softkeys; ALERTS; softkeys place the cursor in the respective list. The; Softkey is enabled only if one or
  • Page 238 – The Direct-to method of navigation, initiated by pressing the; Location of Destination
  • Page 239 – Activation Command; Figure 5-53 Waypoint Submenu; Waypoint Submenu
  • Page 241 – created at the location of the map arrow.
  • Page 242 – Page Menu
  • Page 243 – Figure 5-55 Direct-to Window - Clearing Vertical Constraints
  • Page 244 – Flight Plan Leg Type; Table 5-7 Flight Plan Leg Symbols
  • Page 245 – The following could cause the airway update to fail:; FLIGHT PLAN CREATION; There are three methods to create or modify a flight plan:; Figure 5-56 Active Flight Plan Page
  • Page 246 – Figure 5-57 Active Flight Plan Window on PFD
  • Page 248 – Figure 5-59 Flight Plan Import
  • Page 249 – Figure 5-60 Flight Plan Export
  • Page 250 – ADDING WAYPOINTS TO AN EXISTING FLIGHT PLAN; Figure 5-61 Stored Flight Plan Page; Stored Flight Plan Selected; Figure 5-62 Active Flight Plan Page - FPL Full; Flight Plan Full Message
  • Page 251 – Figure 5-63 Duplicate Waypoints Window
  • Page 252 – ADDING AIRWAYS TO A FLIGHT PLAN; Figure 5-64 Select Airway Page - Selecting Airway
  • Page 253 – Figure 5-65 Select Airway Page - Selecting Exit Point
  • Page 254 – Figure 5-66 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 255 – ADDING PROCEDURES TO A STORED FLIGHT PLAN; Figure 5-67 Stored Flight Plan Page; Flight Plan Name
  • Page 256 – Figure 5-68 Departure Loading Page - Selecting the Departure
  • Page 257 – Figure 5-69 Departure Loading Page - Selecting Transition
  • Page 258 – Figure 5-71 Arrival Loading Page - Selecting the Arrival
  • Page 259 – Figure 5-72 Arrival Loading Page - Selecting the Transition
  • Page 260 – Figure 5-74 Approach Loading Page - Selecting the Approach
  • Page 261 – Figure 5-75 Approach Loading Page - Selecting the Transition
  • Page 262 – FLIGHT PLAN STORAGE; Figure 5-77 Stored Flight Plan Information
  • Page 263 – Individual or all stored flight plans can be deleted from memory.
  • Page 264 – FLIGHT PLAN EDITING; navigation as soon as they are entered.; DELETING THE ACTIVE FLIGHT PLAN
  • Page 268 – ALONG TRACK OFFSETS; Figure 5-78 Along Track Offset
  • Page 269 – PARALLEL TRACK; Figure 5-79 Active Flight Plan Window - Selecting Parallel Track; Selecting Parallel
  • Page 270 – Figure 5-80 Parallel Track Window
  • Page 271 – Figure 5-82 Parallel Track Unavailable; Subdued Prompt; Figure 5-83 Cancelling Parallel Track; Cancel Prompt
  • Page 272 – ACTIVATING A FLIGHT PLAN LEG; Current
  • Page 273 – Figure 5-85 Active Flight Plan Page - New Active Leg; New Active; Confirmation Window; INVERTING A FLIGHT PLAN
  • Page 274 – FLIGHT PLAN VIEWS; Figure 5-86 Active Flight Plan - Leg to Leg vs. Cumulative Distance; Active Flight Plan
  • Page 275 – WIDE
  • Page 276 – CLOSEST POINT OF FPL
  • Page 277 – VERTICAL NAVIGATION; Figure 5-89 Enabling/Disabling Vertical Navigation; ENBL VNV
  • Page 278 – constraint “designated” for vertical guidance. Selecting the; Figure 5-90 Vertical Navigation Direct-To; Current Vertical Navigation Profile; VNV PROF
  • Page 279 – ALTITUDE CONSTRAINTS; Figure 5-91 Waypoint Altitude Constraints
  • Page 280 – Table 5-8 Altitude Constraint Size and Color Coding
  • Page 281 – An altitude constraint is invalid if:
  • Page 283 – DEPARTURES; LOADING A DEPARTURE INTO THE ACTIVE FLIGHT PLAN
  • Page 284 – Figure 5-92 Departure Selection
  • Page 286 – ARRIVALS; LOADING AN ARRIVAL INTO THE ACTIVE FLIGHT PLAN; Figure 5-94 Arrival Selection; Destination Airport
  • Page 287 – Figure 5-95 Arrival Loading; Loaded Arrival
  • Page 288 – APPROACHES; the proper frequency and selecting that NAV receiver on the
  • Page 289 – HSI Annunciation; LNAV; Approach Type; LPV; Table 5-9 Approach Types; LOADING AN APPROACH INTO THE ACTIVE FLIGHT PLAN
  • Page 290 – Figure 5-96 Approach Selection
  • Page 292 – makes the inbound course to the FAF waypoint active.; REMOVING AN APPROACH FROM THE ACTIVE FLIGHT PLAN
  • Page 293 – COURSE TO ALTITUDE; Figure 5-98 Course to Altitude; Course to Alttitude Leg
  • Page 294 – TRIP PLANNING; located in the AUX Page Group.; Figure 5-99 Trip Planning Page
  • Page 295 – waypoints are the endpoints of the selected leg.
  • Page 296 – • Time of; OTHER STATISTICS; Figure 5-100 Trip Planning Page - Flight Plan Mode; Starting and Ending Waypoint; Figure 5-101 Trip Planning Page - Waypoint Mode; Selected Starting and Ending Waypoints
  • Page 297 – plan and leg selection.
  • Page 298 – WEIGHT PLANNING; Figure 5-102 Weight Planning Page; A/C Payload Calculator
  • Page 299 – passenger, and cargo
  • Page 300 – • Estimated landing fuel weight =; WEIGHT CAUTION AND WARNING CONDITIONS; • Estimated fuel at landing weight
  • Page 301 – RAIM PREDICTION; Figure 5-103 RAIM Prediction; Predicting RAIM availability at a selected waypoint:; Knob. The RAIM Prediction ‘WAYPOINT’ field is highlighted.
  • Page 302 – RAIM PREDICTION Box as follows:
  • Page 305 – NAVIGATING A FLIGHT PLAN; should be considered not current.
  • Page 306 – Enter V4 into the flight plan.; Knob to activate the cursor.
  • Page 307 – The desired entry point for V4 (TOP) must be entered. Turn the large; Knob to highlight the desired flight; Figure 5-108 Begin Adding V4 to the Flight Plan; Turn the small; Figure 5-109 Entering V4 Entry Point
  • Page 308 – Figure 5-110 TOP Inserted into the Flight Plan
  • Page 309 – Figure 5-112 List of Available Exits for V4; If necessary, turn either
  • Page 310 – Figure 5-114 V4 is Loaded in the Flight Plan
  • Page 311 – Verify the displayed leg is the desired leg and press the
  • Page 312 – Figure 5-117 Turn on to Active Leg
  • Page 313 – As seen in Figure 5-119, V244 is now the active flight plan leg.
  • Page 314 – Figure 5-120 WIZGE to LAA Leg Active; Figure 5-121 Direct To OPSHN
  • Page 315 – Figure 5-122 Enter VNV Altitude; An altitude of 10,000 feet is entered as requested by ATC.; Figure 5-123 Enter VNV Offset Distance
  • Page 317 – ‘SELECT APPROACH’ should be highlighted as shown in Figure 5-125.; Figure 5-125 Procedures Window; Figure 5-126 List of Available Approaches; Turn either
  • Page 318 – Figure 5-127 List of Available Transitions
  • Page 319 – Figure 5-128 Barometric Minimums Set; With ‘LOAD?’ highlighted, again press the; Key. The selected approach is added to the flight plan as seen; Figure 5-129 Loaded Approach
  • Page 320 – Figure 5-130 Vertical Guidance is Active to the FAF
  • Page 321 – Figure 5-131 Adjusting the Descent
  • Page 322 – Required Vertical
  • Page 323 – Figure 5-134 VDI & RVSI Showing Correctly Established Descent; Align Actual Vertical Speed
  • Page 324 – Figure 5-136 Turn to intercept OPSHN to FSHER Leg
  • Page 325 – Figure 5-137 Tracking the OPSHN to FSHER Leg
  • Page 326 – Figure 5-138 Approaching PYNON
  • Page 327 – Figure 5-139 Approach is Now Active; Figure 5-140 Manually Activate Approach
  • Page 328 – The aircraft altitude is 9,000 feet upon reaching HABUK.; Figure 5-141 Descending Turn to the Initial Approach Fix (IAF)
  • Page 329 – Figure 5-142 Descending to the FAF
  • Page 330 – Figure 5-143 Descending to the Missed Approach Point
  • Page 331 – suspended past the MAP. Press the; Figure 5-144 Missed Approach Active
  • Page 332 – Figure 5-145 Establishing the Holding Pattern
  • Page 333 – ABNORMAL OPERATION; awareness until GPS-derived position data is restored.
  • Page 334 – Figure 5-147 Dead Reckoning Mode - GPS Derived Data Shown in Yellow; or when a 65° bank angle is reached.
  • Page 335 – HAZARD AVOIDANCE; Hazard avoidance features available for the Prodigy; Weather; • GDL 69A SiriusXM Weather (Subscription Optional); Terrain Avoidance
  • Page 336 – SIRIUSXM WEATHER; Weather information to penetrate hazardous weather.; ACTIVATING SERVICES; • The label on the back of the Data Link Receiver
  • Page 337 – Figure 6-1 XM Information Page; USING SIRIUSXM WEATHER PRODUCTS; Knob to select the Map Page Group.
  • Page 338 – Refresh Rate; column in Table; Expiration Time; and its weather suppliers, and are subject to change.
  • Page 339 – SiriusXM Weather Product; no product image; Table 6-1 SiriusXM Weather Product Symbols and Data Timing
  • Page 340 – Table 6-2 SiriusXM Weather Product Display Maps
  • Page 341 – Figure 6-3 Weather Data Link (XM) Page Weather Product Softkeys; Displaying SiriusXM Weather products on the PFD Inset Map:; On the PFD, press the; If the PFD Inset Map is showing the traffic map, press the
  • Page 342 – Setup Menu
  • Page 343 – Figure 6-7 Navigation Map Page Setup Menu
  • Page 345 – data or any radar data to penetrate hazardous weather.
  • Page 347 – No Radar Coverage; Figure 6-11 NEXRAD Legend; indicated in gray shade of purple.; measures the radar reflectivity ratio, or the energy reflected; back to; the radar receiver (; neXraD l; NEXRAD radar images may have certain limitations:; highest; level of NEXRAD data
  • Page 348 – Block Area is 4 km; • Ground clutter
  • Page 349 – • Radar coverage extends to 55oN.; No Coverage Above 55
  • Page 350 – Figure 6-14 Echo Tops Data; Displaying Echo Tops information:; ECHO TOP; Softkey when Echo Tops is selected for; Figure 6-15 Echo Tops Legend
  • Page 351 – are indicated in gray shade of purple.; CLOUD TOPS; Cloud Tops and Echo Tops cannot be displayed at the same time.; Figure 6-16 Cloud Tops Data; Displaying Cloud Tops information:; CLD TOP; Softkey when Cloud Tops is selected for; Figure 6-17 Cloud Tops Legend
  • Page 352 – of the lightning strike is not displayed.; Figure 6-18 SiriusXM Lightning Data; Lightning; Figure 6-19 Lightning Legend
  • Page 353 – Figure 6-20 Cell Movement Data; Storm Cells; •Navigation Map; Figure 6-21 Cell Movement Legend
  • Page 354 – SIGMET (SIGnificant METeorological Information); AIRMET IFR; Figure 6-23 Sample SIGMET Text
  • Page 355 – METARs are shown as colored flags at airports that provide them.; Figure 6-25 METAR Flags on the Weather Data Link Page; Instructions for
  • Page 356 – Figure 6-26 METAR and TAF Text on the Weather Information Page; METAR Text for the
  • Page 357 – Softkey when METARs are selected for display.; Figure 6-27 METAR Legend
  • Page 358 – Forecasts are available for; Figure 6-28 12 Hour Surface Analysis and City Forecast Data; Figure 6-29 Surface Analysis Legend
  • Page 359 – Figure 6-30 Freezing Level Data; Figure 6-31 Freezing Level Legend
  • Page 360 – Softkey when Winds Aloft is; Figure 6-33 Winds Aloft Data with Legend
  • Page 361 – from the; Figure 6-34 County Flood Warning; Figure 6-35 County Warnings Legend
  • Page 362 – Figure 6-36 Cyclone Data Selected for Display; Cyclone; MORE WX; CYCLONE; Softkey when Cyclones are selected to be; Figure 6-37 Cyclone Legend
  • Page 363 – SLD; Softkey when Icing is selected for; Figure 6-39 Icing Potential Legend
  • Page 364 – Softkey when Turbulence is selected; Figure 6-41 Turbulence Legend
  • Page 365 – Figure 6-42 AIREPs and PIREPs on the Weather Data Link (XM) Page
  • Page 366 – Figure 6-43 PIREP Text on the Weather Information Page; Decoded PIREP Text; LEGEND; Softkey when PIREPs or AIREPs are
  • Page 368 – Figure 6-46 Full Text for Selected TFR; product data is removed from the map.; Figure 6-48 Navigation Map Page Setup Menu
  • Page 369 – AIRBORNE COLOR WEATHER RADAR; SYSTEM DESCRIPTION; activity at various altitudes.; PRINCIPLES OF PULSED AIRBORNE WEATHER RADAR; if a target is ten nautical miles away.
  • Page 370 – NEXRAD AND AIRBORNE WEATHER RADAR; Figure 6-50 Radar Beam from a 12 inch Antenna; Figure 6-51 Radar Beam in Relation to the Curvature of the Earth
  • Page 371 – help detect radar shadows.; RADAR SIGNAL REFLECTIVITY
  • Page 372 – Figure 6-52 Precipitation Type and Reflectivity; in between targets, thus obscuring some landmarks.
  • Page 373 – Figure 6-53 Angle of Incidence; SAFE OPERATING DISTANCE; information on safe distance determination.; MAXIMUM PERMISSIBLE EXPOSURE LEVEL (MPEL)
  • Page 374 – Figure 6-54 MPEL Boundary; BASIC ANTENNA TILT SETUP; one way of achieving this.
  • Page 375 – Closely monitor anything that enters the display.; Figure 6-55 Vertical Change in Radar Beam per Nautical Mile
  • Page 376 – WEATHER MAPPING AND INTERPRETATION; WEATHER DISPLAY INTERPRETATION; intensity and rates shown in the table.; 0 dBZ and greater; Table 6-3 Precipitation Intensity Levels; the turbulence is considered severe.
  • Page 377 – Figure 6-56 Cell Irregularities; Steep Gradient; Figure 6-57 The Blind Alley - Horizontal Scan
  • Page 378 – Figure 6-58 The Blind Alley; The Blind Alley at Close Range; may be present if the following characteristics are observed:
  • Page 379 – monitoring essential.; OPERATION IN WEATHER MODE; to Standby mode on landing.; Figure 6-59 Horizontal Scan Display; Radar Mode Scan Line
  • Page 380 – Figure 6-60 Confirming Activating Radar; YES; If
  • Page 381 – adjustment of the Bearing Line.; Figure 6-61 Bearing Line on Horizontal Scan; Bearing Line; RANGE; Knob can also be used to adjust bearing from left to right.
  • Page 382 – Figure 6-62 Vertical Scan Display; Knob can also be used to adjust tilt up and down.
  • Page 383 – Knob can also be used to adjust tilt.; Figure 6-63 Adjusting Tilt on Vertical Scan Display; Scan Line
  • Page 384 – Calibrated Gain; Figure 6-64 Gain Calibration
  • Page 385 – Figure 6-65 Selecting Sector Scan Position
  • Page 386 – 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; WATCH
  • Page 387 – Figure 6-67 Horizontal Scan Without and With WATCH; unwanted weather alerts, deselect the; WX ALRT; Figure 6-68 Weather Alert Indications
  • Page 388 – To activate or deactivate Weather Alerts, select the; Softkey. Activating and deactivating enables; Figure 6-69 Weather Alert on PFD; GROUND MAPPING AND INTERPRETATION; GAIN; TILT; switches to Standby mode upon landing.; Black; 7 dB and greater; Table 6-4 Ground Target Return Intensity Levels
  • Page 389 – STANDBY; (XX indicates number of seconds; * See Table 6-7 for additional failure annunciations; Table 6-5 Radar Modes on the Weather Radar Page; BAD CONFIG
  • Page 390 – situational awareness.
  • Page 391 – DISPLAYING TAWS-B DATA; Table 6-8 TAWS-B Obstacle Colors and Symbology; Warning; Table 6-9 TAWS-B Potential Impact Point Symbols with Alert Types
  • Page 392 – TAWS-B information can be displayed on the following maps:
  • Page 393 – Figure 6-73 Navigation Map Page Setup Menu
  • Page 394 – potential point of impact on the TAWS-B Page.
  • Page 396 – • Press the; Figure 6-77 TAWS-B PFD Alert Annunciation; Alert Annunciation; Figure 6-78 Navigation Map Page
  • Page 397 – Alert Type
  • Page 398 – The purpose of the; Height Above T; “SINK; Figure 6-80 Excessive Descent Rate Alert Criteria; FORWARD LOOKING TERRAIN AVOIDANCE (FLTA); caution or a warning:; Reduced Required Obstacle Clearance (ROC)
  • Page 399 – Figure 6-81 FLTA Minimum Terrain and Obstacle Values; PREMATURE DESCENT ALERTING; ends when the aircraft is 0.5 nm from the runway threshold.; Figure 6-82 PDA Alerting Threshold; Height; PDA ALERTING AREA
  • Page 400 – Figure 6-83 TAWS Alerting Disabled; INHIBIT; FIVE-HUNDRED AURAL ALERT; is to provide an advisory alert of when the aircraft; NEGATIVE CLIMB RATE AFTER TAKEOFF ALERT
  • Page 401 – “DON’T SINK”
  • Page 402 – Table 6-11 TAWS-B System Test Status Annunciations; Select ‘Test TAWS System’ and press the; Key to confirm the selection.
  • Page 403 – Alert Cause; *Annunciation appears on MFD pages when terrain is displayed.
  • Page 405 – DISPLAYING TAWS-A DATA
  • Page 406 – Table 6-13 TAWS-B Obstacle Colors and Symbology; Table 6-14 TAWS-B Potential Impact Point Symbols with Alert Types; is adjustable with the
  • Page 408 – PFD with TAWS-A Annunciations
  • Page 410 – Required
  • Page 411 – Figure 6-92 PDA Alerting Threshold; flta; PDa a; Figure 6-93 TAWS-A Page Menu and Inhibit Annunciation
  • Page 412 – EXCESSIVE DESCENT RATE ALERT; Figure 6-94 Excessive Descent Rate Alert Criteria; EXCESSIVE CLOSURE RATE ALERT
  • Page 413 – active until landing.; FLIGHT INTO TERRAIN ALERT; Flight Into Terrain
  • Page 414 – Figure 6-98 TAWS-A Page Menu and FIT Flap Override Annunciation; Select the TAWS-A Page; FLAP OVR
  • Page 415 – Figure 6-99 FIT Alerting After Takeoff; Negative Climb Rate
  • Page 417 – gPWs a; Figure 6-102 TAWS-A Page Menu and GPWS Inhibit Annunciation; GPWS INH
  • Page 418 – Glideslope Deviation; Radio Altitude; “GLIDESLOPE”; gsD a; GS INH; alert will display a; GP INH
  • Page 419 – Figure 6-104 GSD Alert and PFD Softkeys
  • Page 420 – vertical guidance provided by the flight instruments.; Table 6-11 TAWS-A System Test Status Annunciations
  • Page 421 – TAWS-A ABNORMAL OPERATIONS; message
  • Page 422 – TAWS FAIL; the bank angle is reduced for at least eight seconds.
  • Page 423 – WARNING; TIS is disabled when TCAS I or TCAS II is installed.; Traffic Advisory Off Scale; Table 6-13 TIS Traffic Symbols; at the relative bearing of the intruder.
  • Page 424 – DISPLAYING TRAFFIC DATA; MAP; TRAFFIC; Softkey to display traffic data.; Figure 6-107 TIS Traffic on the Navigation Map Page
  • Page 426 – Figure 6-109 Navigation Map Page Setup Menu; TRAFFIC MAP PAGE
  • Page 427 – Figure 6-111 Traffic Map Page; TIS ALERTS; • A single
  • Page 428 – Inset Map; “TIS Not Available”
  • Page 429 – Traffic Map Page; Data is not being received from the transponder*; DATA FAILED; The transponder has failed*; UNAVAILABLE; TIS is unavailable or out of range; Table 6-14 TIS Failure Annunciations; changed manually using softkeys or the page menu.
  • Page 430 – OPERATING; Table 6-15 TIS Modes; Select the Traffic Map Page.; *Shown as symbol on Traffic Map Page; Table 6-16 TIS Traffic Status Annunciations
  • Page 431 – TIS is disabled when TCAS I is installed.; THEORY OF OPERATION; TCAS I SURVEILLANCE VOLUME
  • Page 432 – Symbol; Relative Altitude; Figure 6-114 Intruder Altitude and Vertical Trend Arrow
  • Page 433 – Sensitivity; Yes; Table 6-18 TA Sensitivity Level and TA Alerting Criteria
  • Page 434 – TCAS I ALERTS; When the GTS 850 detects a new TA, the following occur:; Bearing; Table 6-19 TA Descriptive Voice Announcements
  • Page 435 – SYSTEM TEST; “TCAS System; knob; Figure 6-116 System Test in Progress with Test Pattern
  • Page 436 – OPERATION; displayed and for TAs to be issued.; OPERATE; necessary. Selecting the; Softkey forces the unit into Standby Mode.
  • Page 437 – from 2 to 40 nm, as indicated by the map range rings.; Figure 6-117 Traffic Map Page
  • Page 438 – occurring outside of these limits will always be shown.; iD D
  • Page 439 – Figure 6-118 Traffic Map Page with Flight IDs Enabled; On; Figure 6-119 Traffic Map Page Menu
  • Page 440 – ADDITIONAL TRAFFIC DISPLAYS
  • Page 441 – Figure 6-120 TCAS I Traffic on Navigation Map
  • Page 442 – Figure 6-122 Navigation Map Page Setup Menu; Softkey. A traffic map; Press the softkey again to remove traffic data.
  • Page 443 – TEST; TCAS I Operating; TCAS I Standby; * See Table 6-21 for additional failure annunciations; Table 6-20 TCAS I Modes; NO DATA; Data is not being received from the TCAS I unit; Table 6-21 TCAS I Failure Annunciations
  • Page 444 – maps on which traffic can be displayed.; Table 6-22 TCAS I Traffic Status Annunciations
  • Page 445 – TIS is disabled when TCAS II is installed.; TCAS II SYMBOLOGY; TCAS Symbol; Table 6-23 TCAS II Symbol Description; is still not considered a threat.
  • Page 446 – TCAS II ALERTS; When the TCAS II unit issues a TA or RA, the following occur:; Figure 6-124 Traffic Annunciation with Resolution Advisory (PFD)
  • Page 448 – Figure 6-125 Example Resolution Advisory Visual Cues
  • Page 449 – The TCAS II system can be tested on either the PFD or MFD.; A traffic test
  • Page 450 – on the PFD or on the Traffic Map Page of the MFD.
  • Page 451 – Figure 6-126 Traffic Map Page
  • Page 454 – Figure 6-127 TCAS II Traffic on Navigation Map
  • Page 455 – Figure 6-129 Navigation Map Page Setup Menu
  • Page 456 – (‘TEST MODE’ also shown in white on; TA ONLY; (also shown in white in center of page; FAIL; * Annunciation appears in yellow while in the air.; Table 6-25 TCAS II Modes; Data is not being received from the TCAS II unit; Incorrect data format received from the TCAS II unit; Table 6-26 TCAS II Failure Annunciations
  • Page 457 – Table 6-27 TCAS II Traffic Status Annunciations
  • Page 459 – AUTOMATIC FLIGHT CONTROL SYSTEM; SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM; • GMC 715 AFCS Control Unit; CPL; – Vertical/lateral mode selection and processing
  • Page 461 – Figure 7-1 GMC 715 AFCS Control Unit
  • Page 462 – FLIGHT DIRECTOR OPERATION; ACTIVATING THE FLIGHT DIRECTOR
  • Page 463 – AFCS STATUS BOX; Figure 7-2 PFD AFCS Display
  • Page 464 – FLIGHT DIRECTOR MODES; mode field and flashing for 5 seconds.; Figure 7-3 Loss of VOR Signal; FLIGHT DIRECTOR SELECTION; copilot side, in the center of the AFCS Status Box.; Key again. Pressing the; FD; Figure 7-4 Flight Director Selection Indications; Pilot-side Flight Director Selected
  • Page 465 – COMMAND BARS; Aircraft Symbol
  • Page 466 – ALTS; captured instead of the VNV Target Altitude.; Table 7-2 Flight Director Vertical Modes
  • Page 467 – When the flight director is activated (with the; Altitude Capture Mode is; CHANGING THE PITCH REFERENCE; ressing the; CWS; Figure 7-7 Pitch Hold Mode
  • Page 468 – Figure 7-8 Automatic Mode Transitions During Altitude Capture; Flash Up to 5 sec, Indicating Automatic Transition; CHANGING THE SELECTED ALTITUDE; Bug using the; SPD SEL
  • Page 469 – • Selected; CHANGING THE ALTITUDE REFERENCE; Turning the; flight director’s altitude reference, and does not cancel the mode.; or VNV Target Altitude Capture (ALTV) Mode is active. When the; Key is pressed, the Full Authority; Figure 7-9 Altitude Hold Mode
  • Page 470 – VS; CHANGING THE VERTICAL SPEED REFERENCE; Button; Figure 7-10 Vertical Speed Hold Mode
  • Page 471 – Flight Level Change Mode is selected by pressing the; FLC; Key. This mode acquires and maintains the
  • Page 472 – • Using the; IAS; Table 7-3 FLC Mode Unit Changes
  • Page 473 – Section for more information on VNV flight plans.; VNV ENBL; and cancels any armed VNV modes.; appropriate; Figure 7-13 Vertical Path Tracking Armed Annunciations
  • Page 474 – • Pressing the; VNV; Figure 7-14 Vertical Path Capture
  • Page 475 – Figure 7-15 Vertical Path Tracking Mode
  • Page 476 – revert to Pitch Hold Mode:; Key is pressed while Vertical Path Tracking Mode is; Figure 7-16 Flight Level Change VNV Non-Path Descent
  • Page 477 – after the; Selected Altitude.; Figure 7-17 VNV Altitude Capture; vnv t; on which altitude is to be intercepted first.
  • Page 478 – Figure 7-18 Glidepath Mode Armed; • The active waypoint is at or after the final approach fix (FAF)
  • Page 479 – Figure 7-19 Glidepath Mode
  • Page 480 – Figure 7-20 Glideslope Mode Armed
  • Page 481 – while on the ground by pushing the; Figure 7-22 Takeoff and Go Around Modes
  • Page 482 – Scale of the Attitude Indicator.; Table 7-4 Flight Director Lateral Modes
  • Page 483 – Figure 7-23 Roll Hold Mode Annunciation; Bank Angle; Rolls wings level; Table 7-5 Roll Hold Mode Responses; CHANGING THE ROLL REFERENCE; The roll reference can be changed by pressing the; Button, establishing the desired bank angle, then; LOW BANK MODE; pressing the; BANK; Key while in Heading Select or Navigation Modes (GPS and VOR).; Figure 7-24 Low Bank Mode Limits
  • Page 484 – Heading Select Mode is activated by pressing the; HDG; Key. Heading Select Mode acquires and maintains the; CHANGING THE SELECTED HEADING; Knob synchronizes the Selected Heading to the current heading.; HDG SEL; Knob. Pressing the; Button and hand-flying the; Figure 7-25 Heading Select Mode
  • Page 485 – flight director to enter Navigation Mode.; Figure 7-26 GPS Navigation Mode Armed; • Navigation source manually switched (with the; CHANGING THE SELECTED COURSE; Pressing the
  • Page 486 – Figure 7-27 Navigation Mode
  • Page 487 – flight director to enter Approach Mode.; Key is pressed. Approach Mode acquires and tracks the selected; APR; Key when the CDI is greater; APR; When GPS Approach Mode is armed, Glidepath Mode is also armed.; Figure 7-29 GPS Approach Mode Armed
  • Page 488 – Course is controlled using the; CRS; Knob corresponding to the selected flight director (; INTERCEPTING AND FLYING A DME ARC
  • Page 489 – AUTOPILOT AND YAW DAMPER OPERATION; FLIGHT CONTROL; PITCH AXIS AND TRIM; to reduce the average pitch servo effort.; Switch are operated; MEPT; ROLL AXIS
  • Page 490 – ENGAGING THE AUTOPILOT AND YAW DAMPER; Figure 7-30 Autopilot and Yaw Damper Engaged; Autopilot; CONTROL WHEEL STEERING; holding the; Figure 7-31 CWS Annunciation; Control Wheel Steering; In most scenarios, releasing the
  • Page 491 – DISENGAGING THE AUTOPILOT AND YAW DAMPER; Key does not disengage the yaw damper.; Figure 7-32 Manual Autopilot Disengagement; autopilot disengagement occurs due to:; Figure 7-33 Automatic Autopilot and
  • Page 492 – EXAMPLE FLIGHT PLAN; This scenario-based set of; Figure 7-34 Flight Plan Overview
  • Page 493 – DEPARTURE
  • Page 494 – Figure 7-35 Departure
  • Page 495 – INTERCEPTING A VOR RADIAL; Intercepting a VOR radial:; Figure 7-36 Intercepting a VOR Radial
  • Page 496 – 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 7-37 Transition to GPS Flight Plan
  • Page 497 – DESCENT; Three methods are presented for descent:; Figure 7-38 FLC Descent
  • Page 498 – Select VNV flight control:; Figure 7-39 VPTH Descent
  • Page 499 – Non-path descent using Flight Level Change Mode:; Using the; ,400 feet) at which to level off between VNV flight plan altitudes.
  • Page 501 – APPROACH
  • Page 502 – • Push the; AP DISC; Switch at the decision height and land the aircraft.; KCOS; Figure 7-41 ILS Approach to KCOS
  • Page 503 – Make sure the navigation source is set to GPS (use; Figure 7-42 LPV Approach to KCOS
  • Page 504 – GO AROUND/MISSED APPROACH; Flashes 5 sec
  • Page 506 – AFCS ANNUNCIATIONS AND ALERTS; AFCS CAS MESSAGES; CAS Message; Table 7-6 AFCS CAS Messages; Scrolling Softkey; Figure 7-44 CAS Display
  • Page 507 – AFCS VOICE ALERTS; Voice Alert; “Autopilot”; Switch; Switch malfunction; Table 7-7 AFCS Voice Alerts; OVERSPEED PROTECTION; Airspeed; Figure 7-45 Overspeed Annunciation
  • Page 509 – ADDITIONAL FEATURES; With the availability of SafeTaxi
  • Page 510 – The optional
  • Page 511 – Figure 8-1 Synthetic Vision Imagery; SVS OPERATION
  • Page 512 – Figure 8-2 SVS Softkeys
  • Page 513 – SVS FEATURES; Figure 8-3 SVS on the Primary Flight Display; PATHWAYS
  • Page 514 – Figure 8-4 Programmed and Selected Altitude; Selected; PATHWAY; selected or programmed.
  • Page 515 – selected altitude is lower than the programmed altitude.; Figure 8-5 SVS Pathways, Enroute and Descent
  • Page 516 – in the direction of that leg.
  • Page 517 – represents the aircraft heading.; Flight Path; Figure 8-7 Flight Path Marker and Pathways; ZERO PITCH LINE; when the aircraft is flown at high altitudes.
  • Page 518 – HRZN HDG; APTSIGNS; Figure 8-8 Airport Signs
  • Page 519 – Figure 8-9 Airport Runways
  • Page 520 – Figure 8-10 Terrain Alert
  • Page 521 – airspeed and altitude displays.; Figure 8-11 Obstacle; FIELD OF VIEW; While viewing the Navigation Map Page, press the
  • Page 522 – Figure 8-12 Option Menus
  • Page 523 – configured range. The following is a list of pages where the
  • Page 524 – runway holding lines and taxiways are shown at the cursor.; Figure 8-14 SafeTaxi Depiction on the Navigation Map Page
  • Page 525 – Figure 8-15 Navigation Map PAGE MENU, Map Setup Option; SafeTaxi
  • Page 526 – SAFETAXI DATABASE CYCLE NUMBER AND REVISION; SafeTaxi Database; Power-up Page Display; SafeTaxi database has expired.; Table 8-1 SafeTaxi Annunciation Definitions; on the; MFD1 DB; information by turning the; Knob or pressing the; Key until the SafeTaxi database information is
  • Page 527 – Figure 8-18 AUX – System Status Page, SafeTaxi Current Information; SafeTaxi Data
  • Page 528 – Figure 8-19 AUX – System Status Page, SafeTaxi Database Status; Current Date is before Effective Date
  • Page 529 – CHARTVIEW SOFTKEYS
  • Page 530 – TERMINAL PROCEDURES CHARTS; Navigation Map Page OPTIONS Menu; Figure 8-21 Option Menus; UNABLE TO DISPLAY CHART is then displayed.; Figure 8-23 Unable To Display Chart Banner
  • Page 531 – When a chart is not available by selecting the; Softkey or selecting a Page Menu Option, charts; SHW CHRT; Softkey displays the chart for the nearest airport, if available.; Figure 8-24 Approach Information Page, Chart Selection
  • Page 532 – While the APPROACH Box is selected using the; Knob, the softkeys are blank. Once the desired chart; centers the chart on the screen.; Softkey switches between the DeKalb Peachtree (KPDK) Airport; Figure 8-25 CHRT Softkey, Airport Information Page; Press; CHRT
  • Page 533 – Figure 8-26 Airport Information Page, INFO View, Full Screen Width
  • Page 534 – Key displays the; Softkey displays the Departure Procedure Chart if available.; Chart Not; Figure 8-28 Departure Information Page
  • Page 535 – STAR; Softkey displays the approach chart for the airport if available.; Figure 8-30 Approach Information Page
  • Page 536 – WX; Figure 8-31 Weather Information Page; WX Softkey; A subdued softkey label indicates the function is disabled.; are not available, the; NOTAM; Softkey label appears subdued and is disabled. The; NOTAM; Softkey may appear
  • Page 537 – Figure 8-32 NOTAM Softkey Enabled; Softkey again removes the NOTAMS information.
  • Page 538 – CHART OPTIONS; CHRT OPT; ALL; Softkey shows the entire approach chart on the screen.; Entire Chart; Figure 8-34 Approach Information Page, ALL View; HEADER; Approach; Figure 8-35 Approach Information Page, Header View
  • Page 539 – PLAN; Softkey shows the approach chart two dimensional plan view.; Figure 8-36 Approach Information Page, Plan View; PROFILE; Softkey displays the approach chart descent profile strip.
  • Page 540 – MINIMUMS; Minimum; FIT WIDTH
  • Page 541 – Select; FIT WDTH; Softkey to Show; Figure 8-39 Airport Information Page, FIT WDTH Softkey Selected
  • Page 542 – FULL SCN; Figure 8-40 Airport Information Page, Full Screen and Info Window
  • Page 543 – Figure 8-41 Page Menus; Full Screen On/Off Selection
  • Page 544 – Figure 8-42 Waypoint Information Page, OPTIONS Menu
  • Page 545 – Figure 8-43 Arrival Information Page, Day View
  • Page 546 – CHARTVIEW CYCLE NUMBER AND EXPIRATION DATE; ChartView Database; Table 8-2 ChartView Power-up Page Annunciations and Definitions
  • Page 547 – information by turning the; Knob or pressing the; Key until the ChartView database information is; ChartView; Appendix B for instructions on revising the ChartView database.
  • Page 548 – Figure 8-47 AUX – System Status Page, ChartView Database Status; ChartView Database is Disabled
  • Page 549 – FLITECHARTS SOFTKEYS
  • Page 550 – Figure 8-49 Option Menus; Figure 8-50 Chart Not Available Banner; Figure 8-51 Unable To Display Chart Banner
  • Page 551 – Figure 8-52 Approach Information Page, Chart Selection
  • Page 552 – Knob, the softkeys are blank. Once the desired chart is; page group. In the example shown, the; Softkey switches between the Charlotte, NC (KCLT) Airport; Figure 8-53 CHRT Softkey, Airport Information Page
  • Page 553 – Info Box
  • Page 554 – Key displays the; Figure 8-56 Departure Information Page
  • Page 555 – Figure 8-57 Arrival Information Page; Figure 8-58 Approach Information Page
  • Page 556 – Figure 8-59 Weather Information Page, WX Softkey Selected
  • Page 557 – Softkey shows the entire chart on the screen.; Figure 8-60 Airport Information Page, ALL View Selected
  • Page 558 – Figure 8-61 Approach Information Page, FIT WDTH Softkey Selected
  • Page 559 – Figure 8-62 Airport Information Page, Full Screen and Info Window; Softkey to Switch
  • Page 560 – Figure 8-63 Page Menus
  • Page 561 – Figure 8-64 Waypoint Information Page, OPTIONS Menu
  • Page 562 – Figure 8-65 Approach Information Page, Day View
  • Page 563 – FLITECHARTS CYCLE NUMBER AND EXPIRATION DATE; FliteCharts Database
  • Page 564 – Key until the FliteCharts database information is; FliteCharts
  • Page 565 – instructions on revising the FliteCharts database.; Figure 8-69 AUX – System Status Page, FliteCharts Datbase Status; FliteCharts Expired, but is not Disabled
  • Page 566 – Airport Directory; The Aircraft Owners and Pilots Association (AOPA) and
  • Page 567 – AIRPORT DIRECTORY DATABASE CYCLE NUMBER AND REVISION; Airport Directory Database; Database card contains no Airport Directory data.; Table 8-4 Airport Directory Annunciation Definitions
  • Page 568 – Key until the Airport Directory database information
  • Page 569 – SATELLITE TELEPHONE AND DATA LINK SERVICES; REGISTERING WITH GARMIN FLIGHT DATA SERVICES
  • Page 570 – If necessary, select the; REPORTS; Key. The Page Menu window is now displayed as seen in Figure 8-74.; Figure 8-74 Select Register With GFDS
  • Page 571 – Figure 8-75 Enter Access Code; Enter the Access Code provided by Garmin Flight Data Services.
  • Page 572 – DISABLE/ENABLE IRIDIUM TRANSCEIVER; Figure 8-76 Report Status Page
  • Page 573 – TELEPHONE COMMUNICATION; The pilot or copilot can place and answer calls on the; Figure 8-78 Phone Status Display
  • Page 574 – Internal; Table 8-5 Telephone Symbols
  • Page 575 – Figure 8-79 Incoming Call; Incoming Call Symbol on MFD Page; selecting the; IGNORE; IGNRE ALL; calls and leave the current call unanswered. Selecting the; TEL; Softkey will display the AUX-TELEPHONE
  • Page 576 – Iridium Satellite Network.; Figure 8-80 Initiating a Cabin Call
  • Page 577 – Key again. The cabin phone will now ring as seen in Figure 8-81.; Figure 8-81 Cabin Phone Ringing; select the; HANGUP; Figure 8-82 Cabin Phone Answered
  • Page 578 – Figure 8-83 Initiating an External Call; Figure 8-84 Selecting the Iridium Satellite System
  • Page 579 – Figure 8-85 Enter Phone Number; Figure 8-86 Make the Call
  • Page 580 – Figure 8-87 System is Making the Connection; Figure 8-88 Phone is Answered, Connection Complete
  • Page 581 – HOLD; Softkey again to resume the call.; Figure 8-89 Cockpit Phone on Hold
  • Page 582 – Figure 8-90 Enter Phone Number to Receive Transferred Call
  • Page 583 – Key again to place the call as shown in Figure 8-91.; Figure 8-91 Call Transfer to an External Phone
  • Page 584 – to a call already in progress.; Figure 8-93 Initiate a Conference Call
  • Page 585 – Key again to place the call as shown in Figure 8-94.; Figure 8-94 Conference in External Phone
  • Page 586 – The pilot or copilot can send and receive; Figure 8-96 Text Messaging Page
  • Page 587 – Message Symbol; Table 8-6 Text Message Symbols; VIEWING A TEXT MESSAGE WHEN RECEIVED; -97 will be displayed when a new text message is received.; Figure 8-97 New Text Message Received; New Text Message Pop-up
  • Page 588 – IGNR ALL; Softkey will extinguish; SMS; Softkey will display the; Figure 8-98 Text Message Displayed from Pop-Up Alert; The pop-up alerts may be enabled or disabled through the Page Menu.
  • Page 589 – Figure 8-99 Disabling New Text Message Pop-Ups; REPLY TO A TEXT MESSAGE; After reading a text message, a reply may be sent.
  • Page 590 – Text messages may be sent from the AUX-TEXT MESSAGING Page.; Figure 8-100 Composing a New Text Message
  • Page 591 – a predefined message.; Figure 8-101 Creating/Editing Predefined Messages
  • Page 592 – Figure 8-102 Composing a Predefined Message
  • Page 593 – Figure 8-103 Composing a New Text Message
  • Page 594 – Figure 8-105 Text Message Inbox
  • Page 595 – MANAGING TEXT MESSAGES
  • Page 596 – Figure 8-106 Viewing Message Content
  • Page 599 – Figure 8-108 Desired Network Selected; Figure 8-109 Enter Security Code
  • Page 600 – Figure 8-111 Save Connection
  • Page 601 – Figure 8-112 Select Network to be Edited
  • Page 603 – SYSTEM DATA LOGGING; using any of three data transmission methods (; Figure 8-114 Report Status Page
  • Page 604 – Figure 8-115 Select Transmission Method
  • Page 606 – Figure 8-117 Select Data Within a Specific Time Frame
  • Page 607 – Figure 8-118 Set Starting & Ending Time or Date for Time Frame
  • Page 608 – Figure 8-120 Restore Defaults
  • Page 609 – SIRIUSXM SATELLITE RADIO ENTERTAINMENT; ACTIVATING SIRIUSXM SATELLITE RADIO SERVICES; These IDs are located:
  • Page 610 – RADIO
  • Page 611 – USING SIRIUSXM SATELLITE RADIO; Figure 8-123 XM Radio Page; ACTIVE CHANNEL AND CHANNEL LIST
  • Page 612 – Figure 8-124 Categories List; PRESETS; MORE; the channel list for the Presets category.
  • Page 613 – Figure 8-125 Accessing and Selecting Preset SiriusXM Channels; VOL; brings up the; MUTE; Softkey and the volume increase and decrease softkeys.; Figure 8-126 Volume Control; Radio volume may also be adjusted at each passenger station.
  • Page 615 – Scheduler messages appear in the; Softkey label flashes. Selecting the; Softkey opens the Messages Window and acknowledges the; scheduler message is deleted from the message queue.; Figure 8-128 PFD Messages Window
  • Page 616 – ELECTRONIC CHECKLISTS; Figure 8-129 Checklist Softkeys; checklists from an; Softkey is not available.
  • Page 617 – Figure 8-130 Sample Checklist
  • Page 618 – Figure 8-131 Emergency Checklist Page Example
  • Page 619 – ABNORMAL OPERATION; SVS TROUBLESHOOTING; Figure 8-132 SVS Reversionary Mode
  • Page 620 – extreme pitch attitudes.; Figure 8-133 Unusual Attitude Display; Blue Band; Figure 8-134 Blue Sky Bar with Full Display Terrain; Terrain
  • Page 621 – GDL 69/69A DATA LINK RECEIVER TROUBLESHOOTING; SiriusXM Satellite Radio; Selecting the System Status Page:; Knob to select the AUX Page Group.; Figure 8-135 LRU Information Window on System Status Page
  • Page 622 – Table 8-7 GDL 69/69A Data Link Receiver Error Messages
  • Page 623 – APPENDIX A; ANNUNCIATIONS AND ALERTS; which repeats until acknowledged.; CAUTION MESSAGES; tone which repeats until acknowledged.
  • Page 624 – E1 FAIL
  • Page 626 – See the Airplane Flight Manual (AFM) for recommended pilot actions.
  • Page 628 – COMPARATOR ANNUNCIATIONS; Figure A-1 Sensor Comparator Window; Comparator; Comparator Window Text; Difference in altitude sensors is > 200 ft.; IAS MISCOMP; No data from one or both altitude sensors.; IAS NO COMP; No data from one or both airspeed sensors.; HDG NO COMP; No data from one or both heading sensors.; PIT NO COMP; No data from one or both pitch sensors.; ROL NO COMP
  • Page 629 – REVERSIONARY SENSOR ANNUNCIATIONS; SENSOR; Figure A-2 Reversionary Sensor Windows; Reversionary; Reversionary Sensor
  • Page 630 – When a new message is issued, the
  • Page 631 – Figure A-4 System Failure Annunciations; System Annunciation; Attitude and Heading Reference System is aligning.
  • Page 632 – Display system is not receiving valid heading input from AHRS.; System Annunciation section.
  • Page 638 – GSD1 CONFIG
  • Page 646 – Terrain or Obstacle database; NO GPS; TAWS-A ALERT AVAILABILITY
  • Page 647 – TAWS-B SYSTEM STATUS ANNUNCIATIONS; TAWS TEST; TERRAIN DATABASE FAILURE
  • Page 648 – TCAS I ALERTS AND ANNUNCIATIONS; TCAS I Modes; TCAS I Traffic Status Annunciations
  • Page 649 – TCAS II ALERTS AND ANNUNCIATIONS; TCAS II Modes; RA OFF SCALE; TCAS II Traffic Status Annunciations
  • Page 650 – OTHER PRODIGY; FLIGHT PLAN IMPORT/EXPORT MESSAGES; Flight Plan Import/Export Results
  • Page 651 – PILOT PROFILE IMPORT/EXPORT MESSAGES; Pilot Profile Import/Export Results
  • Page 653 – APPENDIX B; DATABASE MANAGEMENT; JEPPESEN DATABASES; this database had been referred to as the ‘aviation database’.
  • Page 654 – Figure B-1 Standby Navigation Database Prompt; DUAL NAVIGATION DATABASE FEATURE
  • Page 655 – Loading a standby navigation database:; Turn the system ON. A prompt similar to the following is displayed.; Figure B-3 Standby Navigation Database Prompt; Figure B-4 Standby Navigation Database Update Complete
  • Page 656 – Figure B-5 Navigation Database Verification Prompt
  • Page 657 – GARMIN DATABASES; Figure B-7 Correct Database Locations; MFD; database versions must be kept in each display unit.
  • Page 659 – Figure B-9 Synchronization Error Message; Database Synchronization Error Message; Error Message; Table B-1 Database Synchronization Error Messages; UPDATING GARMIN DATABASES; • Updated database obtained from the Garmin website
  • Page 660 – Figure B-10 Database Information on the Power-up Screen; Unselected
  • Page 661 – Figure B-12 GRS1 Magnetic Field Variation Database Update Prompt; Loading the magnetic field variation database update:; Key on the MFD. A progress monitor is displayed; Figure B-13 Uploading Database to GRS1
  • Page 662 – With ‘OK’ highlighted, press the; When the upload is complete, the system is ready for use.; Figure B-15 Uploading Database to GRS2
  • Page 663 – APPENDIX C; GLOSSARY
  • Page 669 – APPENDIX D; FREQUENTLY ASKED QUESTIONS; on GPS for all phases of flight.; sBas; performs the following functions:
  • Page 670 – “/G” may be filed for a flight plan. The Prodigy; oBs s
  • Page 672 – after
  • Page 673 – APPENDIX E; GENERAL TIS INFORMATION; INTRODUCTION; Aircraft without an operating transponder are invisible to TIS.; TIS LIMITATIONS; comprehensive explanation.
  • Page 674 – The following errors are common examples:
  • Page 675 – APPENDIX F; NAVAIDS; Item; LINE SYMBOLS; Item; DISPLAY SYMBOLS; for SiriusXM Weather Product legends.
  • Page 677 – Terrain more than 1000 ft below the aircraft altitude; TAWS Color Chart; Obstacle Symbol; Red; Obstacle Symbols and Colors
  • Page 678 – Feature
  • Page 679 – INDEX
  • Page 681 – Flight plan
  • Page 682 – Messages
  • Page 683 – Procedures
  • Page 685 – VNV guidance
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Embraer Phenom 100

Embraer Prodigy

®

Flight Deck 100

Pilot’s Guide

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Summary

Page 4 - ii; LIMITED WARRANTY

Embraer Prodigy ® Flight Deck 100 Pilot’s Guide 190-00728-04 Rev. A ii LIMITED WARRANTY LIMITED WARRANTY Within the warranty period, Garmin will, at its sole discretion, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer fo...

Page 5 - iii

190-00728-04 Rev. A Embraer Prodigy ® Flight Deck 100 Pilot’s Guide iii WARNINGS, CAUTIONS, AND NOTES WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature. The terrain avoidance feature is NOT intended to be used as a primary reference for t...

Page 6 - iv; Aeronautical; Information

Embraer Prodigy ® Flight Deck 100 Pilot’s Guide 190-00728-04 Rev. A iv WARNINGS, CAUTIONS, AND NOTES WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the ac...

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