Garmin Software Version 0734.23- User Manual

Garmin Software Version 0734.23

Garmin Software Version 0734.23– User 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 8 – Because of variation in the earth’s magnetic field, operating the
  • Page 9 – This product, its packaging, and its components contain chemicals
  • Page 10 – Blank Page
  • Page 11 – record of revisions; part number; Initial release; revision date of revision Affected pages; All
  • Page 13 – table of Contents
  • Page 14 – ii
  • Page 15 – iii
  • Page 16 – iv
  • Page 17 – Flight instruments; seleCting the Altimeter bArometriC pressure setting
  • Page 18 – ChAnge nAvigAtion sourCes
  • Page 19 – turn vspeed bugs on or oFF bY CAtegorY
  • Page 21 – engine & Airframe systems; engine & AirFrAme sYstems; engine indiCAtion sYstem
  • Page 22 – Engine Indications; thrust rating; Indication; Cruise; CLB; Climb; Continuous; TO; Takeoff; GA; Go Around; Thrust Rating Indications; Selecting a thrust rating:; Select the; Select the; ENG SET; Softkey; CON
  • Page 23 – Automatic thrust reserve; Description; ATR enabled in both engines; ATR; ATR armed in both engines, but inactive; * When no indication is shown, ATR has not been enabled or armed; or
  • Page 24 – takeoff data set Window; Takeoff Data Set Window; Fuel and electrical indications; Fuel Display; Total Fuel Quantity; Electrical Display
  • Page 25 – Cabin pressurization; Cabin Pressure Display; Setting the displayed landing field elevation:; spoiler and landing gear; Spoiler and Landing Gear
  • Page 26 – Landing Gear Down; Landing Gear Position Indications; Invalid information; SPDBRK; Spoiler retracted; GND SPLR; Speedbrakes deployed; Spoiler Indications
  • Page 27 – Flaps and trim; Flap and Trim Indications; sYnoptiCs; System Status Synoptics Page
  • Page 28 – Environmental Control System Synoptics Page
  • Page 29 – Unit; Fan; Environmental Control System Unit Status Indications
  • Page 30 – electrical; Battery; Electrical Synoptics Page; Bus
  • Page 31 – Generator; Electrical System Unit Status Indications
  • Page 32 – Fuel; Fuel Synoptics Page
  • Page 33 – Fuel Line; Fuel System Unit Status Indications
  • Page 34 – ice protection system; Ice Protection Synoptics Page
  • Page 35 – Anti Ice Line; Ice Protection System Unit Status Indications
  • Page 37 – enter or ChAnge Flight id
  • Page 39 – seleCting A nAv rAdio; INTR COM
  • Page 40 – Knob controls only the volume (pressing the; CleArAnCe reCorder And plAYer
  • Page 41 – AFCs; AutomAtiC Flight Control sYstem; Flight direCtor ACtivAtion; *Valid VNV flight plan must be entered before
  • Page 42 – vertiCAl modes; ALTS; is to be captured instead of VNAV Target Altitude
  • Page 43 – lAterAl modes; green along the Roll Scale of the Attitude Indicator.
  • Page 44 – Press the; CSC
  • Page 45 – gps navigation; gps nAvigAtion; direct-to navigation using the mFd
  • Page 46 – ACtivAte A stored Flight plAn; Knob
  • Page 47 – stop nAvigAting A Flight plAn; FPL
  • Page 48 – CLR
  • Page 49 – Flight planning; Flight plAnning; Weight plAnning; All procedures apply to the MFD unless otherwise stated.; entering Weight parameters; Turn the large; entering Fuel parameters
  • Page 50 – The page mode must be set to ‘MANUAL’ to perform the following
  • Page 51 – ent; CreAte A neW user WAYpoint deFined bY lAtitude & longitude
  • Page 52 – CreAte A neW user WAYpoint deFined bY rAdiAls From other
  • Page 54 – CreAte A neW user WAYpoint deFined bY A rAdiAl & distAnCe From
  • Page 55 – delete A user WAYpoint
  • Page 56 – CreAte A neW Flight plAn; When creating a new flight plan in the Active Flight Plan Window,; using the mFd; using the pFd
  • Page 57 – import A Flight plAn From An sd CArd; insert A WAYpoint in the ACtive Flight plAn
  • Page 58 – enter An AirWAY in A Flight plAn
  • Page 59 – invert An ACtive Flight plAn; Key; remove A depArture, ArrivAl, ApproACh, or AirWAY From A Flight
  • Page 60 – store A Flight plAn
  • Page 61 – invert And ACtivAte A stored Flight plAn; CopY A Flight plAn; delete A Flight plAn
  • Page 62 – grAphiCAl Flight plAn CreAtion; ABOVE; export A Flight plAn to An sd CArd
  • Page 63 – procedures; proCedures; loAd And ACtivAte A depArture proCedure; ACtivAte A depArture leg
  • Page 64 – ACtivAte An ArrivAl leg
  • Page 65 – FMS; ENT; ACtivAte An ApproACh in the ACtive Flight plAn
  • Page 66 – ACtivAte A missed ApproACh in the ACtive Flight plAn; PROC
  • Page 67 – hazard Avoidance; hAzArd AvoidAnCe; Customizing the hAzArd displAYs on the nAvigAtion mAp; Menu; Use of XM weather for hazardous weather penetration is not; displaying xm Weather on the navigation map page; displaying Weather on the Weather data link page
  • Page 68 – map panning information – Weather data link page
  • Page 69 – If the system is configured to use the optional TCAS II, TIS is not; (intruder is beyond 5 nm and greater than 1200’ vertical separation); Traffic Symbol Description; displaying traffic on the traffic map page; displaying traffic on the navigation map
  • Page 70 – If the system is configured to use TIS, the optional TCAS II is not; Traffic Symbol; system test
  • Page 71 – Changing the Altitude range
  • Page 72 – The TAWS display shows supplemental information only. It should; Manual System Test
  • Page 73 – Red; Enable/Disable Aviation Data; inhibiting/enabling FltA and pdA Alerting; Only available during a GSD alert.
  • Page 75 – Inhibit TAWS; Displaying Terrain and Obstacles on the Navigation Map
  • Page 76 – Airborne Color WeAther rAdAr; Begin transmitting only when it is safe to do so. If it is desired to; displaying Weather on the Weather radar page; Adjusting Antenna tilt; Move the
  • Page 77 – Adjusting Antenna bearing; Adjusting gain; Changing the gain in Weather Mode will cause precipitation
  • Page 78 – To activate or deactivate the; WATCH; feature is only available in the Horizontal Scan Mode.; WX ALRT; Softkey. Activating
  • Page 79 – Additional Features; AdditionAl FeAtures; Use appropriate primary systems for navigation, and for terrain,; to the Prodigy; displaying synthetic terrain; PFD; SYN VIS; SYN TERR; BACK; Softkey to return to the previous page.
  • Page 80 – displaying pathways; When the optional TCAS II system issues a Resolution Advisory (RA); displaying heading on the horizon
  • Page 81 – terminAl proCedure ChArts; With the availability of SafeTaxi; safetaxi; SafeTaxi; FliteCharts
  • Page 82 – view Charts from the navigation map page; view Charts from the Active Flight plan page
  • Page 83 – AopA Airport direCtorY
  • Page 84 – Selecting the; muting incoming Call Alerts; To exit the call, select the
  • Page 85 – placing a Call on hold; Control and monitoring of; viewing the Wi-Fi setup page
  • Page 86 – setting up a new Wi-Fi Connection
  • Page 87 – editing a saved network
  • Page 88 – make full use of the System Data Logging feature.; viewing the report status page
  • Page 89 – enable/disable periodic send for periodic test reports
  • Page 90 – The XM
  • Page 91 – entering a Channel directly; Up to 15 channels from any category can be assigned a preset number.; Adjusting volume
  • Page 92 – The system accesses the checklists from an; The following colors are used for checklist items:; checked; Accessing and navigating Checklists
  • Page 93 – immediately Accessing emergency procedures
  • Page 95 – Abnormal operation; AbnormAl operAtion; The Embraer Phenom 300 Airplane Flight Manual (AFM) always takes; engine; failed engine (“E1 FAIL” or “E2 FAIL”), the corresponding; Engine Failure Indication; CAbin pressurizAtion; Cabin Leak Indication
  • Page 96 – text. The CAS message “OXY LO PRES” is also issued.; FlAps; The following denote abnormal flap conditions:; at Takeoff
  • Page 97 – Rudder; Outside Takeoff; reversionArY mode; – By pressing the; – By pressing the; DISPLAY BACKUP; – By pressing the; DISPLAY BACKUP; AbnormAl Com operAtion; In the event of a failure of both PFDs,
  • Page 98 – Audio is not available on the speakers in case of an Audio Panel and; hAzArd displAYs With loss oF gps position; Loss of Hazard Functions with Loss of GPS; unusuAl Attitudes; The PFD ‘
  • Page 99 – Box; deAd reCkoning; Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic
  • Page 100 – message appears on the PFD.; Symbolic Aircraft
  • Page 101 – As a result of operating in
  • Page 103 – Annunciations & Alerts; AnnunCiAtions & Alerts; CAs messAges; by a triple chime tone which repeats until acknowledged.; Caution messages; by a single chime tone which repeats until acknowledged.
  • Page 104 – Message
  • Page 107 – See the Airplane Flight Manual (AFM) for recommended pilot actions.
  • Page 109 – ALT NO COMP; reversionArY sensor AnnunCiAtions
  • Page 110 – reversionary; Alert Type
  • Page 112 – TAWS FAIL
  • Page 113 – TAWS-A Alert Type Available; RTC
  • Page 115 – TAWS TEST
  • Page 116 – None; TEST; shown in white on top; TA ONLY; (also shown in white in; FAIL; * Annunciation appears yellow while in flight.; tCAs ii Failure Annunciations; NO DATA; Data is not being received from the TCAS II unit; DATA FAILED; Incorrect data format received from the TCAS II unit
  • Page 117 – Traffic Status Banner; RA OFF SCALE
  • Page 119 – Flight Plan Import/Export
  • Page 125 – – GMA1 software; giA 63W messAge Advisories
  • Page 139 – Appendix; pFd soFtkeY mAp; Top Level PFD Softkeys; CAS
  • Page 140 – INSET Map Softkeys
  • Page 141 – SENSOR Softkeys; SENSOR
  • Page 142 – PFD Configuration Softkeys; Displays the softkeys for enabling or
  • Page 144 – Transponder Softkeys
  • Page 145 – altitude interrogations)
  • Page 146 – Transponder/Traffic Softkeys with TCAS II Option; Displays the transponder and
  • Page 147 – Displays the TCAS control
  • Page 148 – Displays
  • Page 149 – mFd soFtkeY mAp; SYSTEM Softkeys; Disabled when aircraft is on the ground.
  • Page 150 – Accesses softkeys for manually setting the
  • Page 151 – MAP Softkeys
  • Page 152 – Selects desired amount of map detail cycles; duAl nAvigAtion dAtAbAses; YES
  • Page 153 – AutomAtiC dAtAbAse sYnChronizAtion; The 9-arc second terrain database may take as long as 100 minutes to; synchronizing databases
  • Page 154 – synchronization when ‘Card Full’; Error Message; The; Canceling database synchronization
  • Page 155 – index
  • Page 156 – Landing gear status 5, 9
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Embraer Prodigy

™

Flight Deck 300

Cockpit Reference Guide

Embraer Phenom 300

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Summary

Page 8 - Because of variation in the earth’s magnetic field, operating the

Cockpit Reference Guide for the Prodigy ™ Flight Deck 300 190-00761-00 Rev. A Warnings, Cautions & notes WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according to local, state, or federal laws. For more information, refer to our website at www...

Page 9 - This product, its packaging, and its components contain chemicals

Cockpit Reference Guide for the Prodigy ™ Flight Deck 300 190-00761-00 Rev. A Warnings, Cautions & notes NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin accurately processes and cross-validates the data, but cannot guarantee the accuracy and ...

Page 10 - Blank Page

Cockpit Reference Guide for the Prodigy ™ Flight Deck 300 190-00761-00 Rev. A Warnings, Cautions & notes Blank Page

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