Garmin Software Version 0369.13- User Manual

Garmin Software Version 0369.13

Garmin Software Version 0369.13– 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 9 – RECORD OF REVISIONS; Part Number
  • Page 10 – Revision Date of Revision Affected Pages
  • Page 11 – TABLE OF CONTENTS; Section 1: System Overview
  • Page 12 – ii; Section 7: Navigation
  • Page 13 – iii; Section 11: Abnormal Operation
  • Page 14 – iv; Blank Page
  • Page 15 – SECTION 1: SYSTEM OVERVIEW; The purpose of this Cockpit Reference Guide is to; The pilot should read and thoroughly
  • Page 16 – MFD Only
  • Page 19 – Softkey OFF; Figure 1-3 INSET Softkeys; INSET
  • Page 20 – Figure 1-4 PFD Configuration Softkeys; PFD
  • Page 21 – OBS; XPDR
  • Page 22 – Figure 1-6 MFD Softkeys
  • Page 23 – Figure 1-7 Page Group Icon; Turn the large; Knob; FMS; Knob; to select pages within the
  • Page 24 – VERTICAL NAVIGATION; All arrival procedure altitudes contained in
  • Page 25 – White Text; Table 1-1 VNV Altitude Text Size and Color; Refer to Figure 1-8 and Table 1-1 for more detail; Figure 1-8 VNAV Altitudes; Some altitudes retrieved from the database have; Figure 1-9 Altitude Restrictions; See Section 7 - Navigation, for a sample flight plan
  • Page 26 – Figure 1-10 PFD Setup Menu Window; and; DATABASE UPDATES; Jeppesen Aviation Database; After the aviation database is installed,; Updating the Jeppesen aviation database:; Figure 1-11 Database Update Prompt
  • Page 27 – Figure 1-12 Database Update Confirmation; Garmin Databases; Since these databases are not stored internally in; The data contained in the terrain and; ENT
  • Page 29 – SECTION 2: FLIGHT INSTRUMENTS; Figure 2-1 Default PFD Information
  • Page 30 – Figure 2-2 Additional PFD Information; Flight Plan Messages/Indications
  • Page 31 – AIRSPEED INDICATOR; Figure 2-4 Airspeed Indicator; Speed Indication; Figure 2-5 Red Pointer at Vne; Speed Ranges; ATTITUDE INDICATOR; Figure 2-6 Attitude Indicator
  • Page 32 – Figure 2-7 Altimeter; Selected Altitude Bug; The Selected Altitude Bug is displayed at the Selected; Set the Selected Altitude Bug:; Altitude Trend Vector; The end of the trend vector displays approximately; Barometric Setting Box; Select barometric pressure:; Altitude Alerting; Figure 2-8 Altitude Alerting Visual Annunciations; Visual annunciations appear in the Altitude Reference
  • Page 33 – The LOW ALT annunciation is not available; When the Final Approach Fix (FAF) is the active; Figure 2-10 Low Altitude on GPS Approach; Low Altitude
  • Page 34 – GLIDESLOPE INDICATOR; The Vertical Deviation and Required Vertical Speed; Figure 2-11 Vertical Deviation Indications; Figure 2-12 Glidepath Indicator; The Glideslope Indicator appears when an ILS is tuned; Figure 2-13 Glideslope Indicator
  • Page 35 – MARKER BEACON ANNUNCIATIONS; Figure 2-14 Marker Beacon Annunciations; VERTICAL SPEED INDICATOR; Figure 2-15 Vertical Speed Indicator; VS; BAROMETRIC ALTITUDE MINIMUMS; Figure 2-16 Barometric Minimum Descent Altitude Settings; Set the barometric altitude minimums:
  • Page 36 – Altitude Reached; Figure 2-17 Barometric Minimum Descent Altitude; Barometric; HORIZONTAL SITUATION INDICATOR
  • Page 37 – Tick marks to the left and right of the lubber line; Figure 2-20 Standard-Rate Turn Indication; Course Pointer; The course pointer is a single line arrow (GPS, VOR1; Figure 2-21 Course Pointer; The CDI scale automatically adjusts to the current; Flight Phase; depending on variables (see Figure
  • Page 38 – Figure 2-22 Phases of Flight/CDI Scaling; Figure 2-23 Typical LNAV and LNAV+V Approach CDI Scaling; Figure 2-24 Typical LNAV/VNAV and LPV Approach CDI Scaling
  • Page 39 – Figure 2-25 HSI with Bearing Information; Figure 2-28 DME Information Window; Navigation Source; Change CDI navigation sources:; CDI
  • Page 40 – • SUSP – Displayed when in OBS Mode indicating; The; Softkey is only displayed when; When the window is selected for display, but wind; Option 1; Figure 2-30 Wind Data Window; Displaying wind data:
  • Page 41 – Figure 2-31 Timer Status Prompts; Change the Generic Timer:
  • Page 43 – SECTION 3 – ENGINE; SECTION 3: ENGINE INDICATION; The Engine Instrument Display is displayed on the left; Figure 3-1 Engine Instrument Display on the MFD
  • Page 44 – ENGINE; Fuel Totalizer; DEC FUEL
  • Page 46 – LEAN
  • Page 49 – TRANSPONDER; The NAV/COM controls and frequency boxes are
  • Page 50 – Figure 4-2 Frequency Fields
  • Page 51 – RADIO STATUS INDICATIONS; Figure 4-5 Radio Status Indications; AUTOMATIC SQUELCH; COM; OPTIONAL NAV RADIOS; DME
  • Page 52 – Change the DME tuning source:; Figure 4-9 DME Selection Window; Auto-tuning on the PFD; NRST; Auto-tuning on the MFD; Figure 4-11 Ground Mode
  • Page 53 – STBY; Code Number and; Figure 4-12 Standby Mode; Manual ON Mode; ON; ON Mode; ALT; Figure 4-14 Altitude Mode; Reply Status; Figure 4-15 Reply Indication; Reply; Code Selection; VFR Code Selection; The pre-programmed VFR Code is set at; Enter Code Using Softkeys
  • Page 54 – Enter Code Using the FMS Knob; Flight ID Reporting; If so configured, the Flight ID may be entered in the
  • Page 55 – SECTION 5 – AUDIO PANEL; SECTION 5: AUDIO PANEL; Figure 5-1 Audio Panel Controls
  • Page 56 – COM RADIO SELECTION; Figure 5-2 Transceivers; MARKER BEACON RECEIVER; Figure 5-3 Marker Beacon Annunciators on the PFD; Marker Beacon Signal Sensitivity; Figure 5-4 Marker Beacon; NAV RADIO AUDIO SELECTION; Figure 5-5 Navigation Radios
  • Page 57 – PILOT; Figure 5-6 ICS Isolation; INTERCOM SQUELCH CONTROL; MAN SQ
  • Page 58 – DIGITAL CLEARANCE RECORDER; PLAY
  • Page 59 – SECTION 6: AUTOMATIC FLIGHT; Figure 6-1 AFCS Keys; AP DISC (Autopilot Disconnect) Button; FLIGHT DIRECTOR OPERATION
  • Page 60 – FD; Figure 6-2 PFD AFCS Display; Command Bars; Figure 6-3 Command Bars
  • Page 61 – FLIGHT DIRECTOR MODES; Figure 6-4 Loss of VOR Signal; Pitch Modes
  • Page 62 – Table 6-1 lists the pitch modes with their corresponding; ALTS; Table 6-1 Flight Director Pitch Modes
  • Page 63 – Figure 6-5 Pitch Hold Mode; Changing the Pitch Reference
  • Page 64 – Figure 6-6 Automatic Mode Transitions During Altitude Capture; Flash Up to 10 sec, Indicating Automatic Transition; Changing the Selected Altitude; Pressing the; Button while in Selected; Turning the; Knob while in Altitude; CWS
  • Page 65 – If the Selected Altitude is reached during CWS; Figure 6-7 Altitude Hold Mode; In Vertical Speed Mode, the flight director acquires
  • Page 66 – Figure 6-8 Vertical Speed Mode; Changing the Vertical Speed Reference; The Selected Altitude should be set before; FLC
  • Page 67 – Changing the Airspeed Reference; Figure 6-9 Flight Level Change Mode
  • Page 68 – Figure 6-10 Vertical Path Tracking Armed Annunciations; VNV
  • Page 69 – In conjunction with the “TOD [top of descent] within 1; Figure 6-11 Vertical Path Capture
  • Page 70 – Figure 6-12 Vertical Path Tracking Mode; Automatic Pitch Hold Reversion
  • Page 71 – Figure 6-13 Flight Level Change VNAV Non-Path Descent; Armed VNAV Target Altitude and Selected; Flash up to 10 sec, Indicating Automatic Transition; Figure 6-14 VNAV Altitude Capture; Changing the VNAV Target Altitude; Button while in VNAV
  • Page 72 – Button while Glidepath; Figure 6-15 Glidepath Mode; APR
  • Page 73 – Figure 6-16 Glidepath Mode Armed; If vertical guidance becomes or is expected to become; Button while Glideslope; Figure 6-17 Glideslope Mode; Glideslope Mode is available for LOC/ILS approaches; Figure 6-18 Glideslope Mode Armed; Once the localizer has been set as the navigation
  • Page 74 – Figure 6-19 Go Around Mode; Roll Modes
  • Page 75 – If Roll Hold Mode is activated as a result; Changing the Roll Reference
  • Page 76 – Heading Select Mode is activated by pressing; HDG; Knob synchronizes the; The Selected Heading is adjusted using the; Figure 6-21 Heading Select Mode; Turns are commanded in the same direction as Selected
  • Page 77 – The selected navigation receiver must have; Figure 6-22 Navigation Mode; Course and deviation.; NAV; Figure 6-23 GPS Navigation Mode Armed
  • Page 78 – Changing the Selected Course
  • Page 79 – AUTOPILOT OPERATION; Refer to the AFM for specific instructions; Engaging the Autopilot; Autopilot engagement/disengagement is; Button to disengage the; AP; Figure 6-25 Autopilot Engaged; Autopilot Engaged; Control Wheel Steering; Control Wheel Steering
  • Page 80 – Figure 6-27 Automatic Autopilot Disengagement; Autopilot Automatically Disengaged; Figure 6-28 Manual Autopilot Disengagement; Autopilot Manually Disengaged
  • Page 81 – EXAMPLE PROCEDURES USING AFCS; The diagrams in this section are for instruc-; This section provides a scenario-based set of; Figure 6-29 Flight Plan Overview
  • Page 82 – Figure 6-30 Departure
  • Page 83 – During climb-out, the autopilot continues to fly the; Intercepting a VOR radial:; Arm VOR Navigation Mode:; e CDI; Softkey to set the navigation; CRS; Knob to set the Selected Course to; Figure 6-31 Intercepting a VOR Radial; Key. This arms VOR Navigation
  • Page 84 – Changing the navigation source cancels; As the aircraft approaches the Salina VOR, GPS is used; Flying a GPS flight plan:; Transition from VOR to GPS Navigation Mode:; Softkey until GPS is the selected; Key to activate GPS Navigation; Figure 6-32 Transition to GPS Flight Plan
  • Page 85 – While flying the arrival procedure, the aircraft is; Flight Level Change descent:; Select Flight Level Change Mode:; Knob, set the Selected Altitude to; Figure 6-33 FLC Descent; Key to activate Flight Level Change
  • Page 86 – Figure 6-34 VPTH Descent
  • Page 87 – Knob, set the Selected Altitude; Key before the planned TOD
  • Page 88 – Flying an ILS approach:; KCOS; Figure 6-36 ILS Approach to KCOS
  • Page 89 – Flying a WAAS precision approach:; Figure 6-37 LPV Approach to KCOS
  • Page 90 – Flying a missed approach:; Flashes 5 sec; As a result of calculations performed by
  • Page 91 – AFCS ANNUNCIATIONS AND ALERTS; AFCS Status Alerts; The following annunciations (listed in order of; Figure 6-39 AFCS Status Annunciation; AFCS Status; Table 6-4 AFCS Status Field Alerts
  • Page 92 – Overspeed protection is provided in situations where; Figure 6-40 Overspeed Annunciation; Airspeed
  • Page 93 – SECTION 7 – NAVIGATION; SECTION 7: NAVIGATION; The majority of the following discussions pertain to; NAVIGATION MAP PAGE; The map display should only be; Select the MAP Page Group; Direct-to Navigation from the MFD; Enter a Direct-to Destination
  • Page 95 – Manually Define the Active Direct-to; Figure 7-6 Canceling Direct-to Navigation; Direct-to Navigation from the PFD
  • Page 97 – Cancelling Direct-to Navigation; NAVIGATING AN EXAMPLE FLIGHT; The following discussion is an example of navigating a; If the loaded arrival procedure has
  • Page 99 – Figure 7-13 Begin Adding V4 to the Flight Plan
  • Page 100 – Figure 7-16 List of Available Airways for TOP
  • Page 101 – Figure 7-19 V4 is Loaded in the Flight Plan; Figure 7-20 Confirm Active Leg; Figure 7-21 V4 Now Active Leg
  • Page 102 – Figure 7-22 Turn on to Active Leg
  • Page 103 – Figure 7-25 HYS to LAA Leg Active; Figure 7-26 Direct To OPSHN; Figure 7-27 Enter VNV Altitude
  • Page 104 – Figure 7-28 Enter VNV Offset Distance; PROC
  • Page 105 – b) ‘SELECT APPROACH’ should be highlighted as; Figure 7-30 Procedures Window; Key. A list of available approaches; Figure 7-31 List of Available Approaches; Knob to select the LPV approach; Key. A list of available transitions; Figure 7-32 List of Available Transitions; Knob to select the desired
  • Page 106 – Figure 7-33 Loaded Approach; Figure 7-34 Vertical Guidance is Active to the FAF
  • Page 107 – VNV PROF; Figure 7-35 Adjusting the Descent
  • Page 108 – Upon reaching TOD, a descent vertical speed is; Figure 7-38 VDI & RVSI Showing Correctly Established Descent; When the aircraft is one minute from the bottom of; Figure 7-40 Turn to intercept OPSHN to FSHER Leg
  • Page 109 – After passing OPSHN, the next leg of the arrival; Figure 7-41 Tracking the OPSHN to FSHER Leg; The flight continues through the arrival procedure; Figure 7-42 Approaching PYNON
  • Page 110 – Upon passing PYNON the approach procedure will; Figure 7-43 Approach Leg is Now Active; Knob to highlight ‘ACTIVATE; Figure 7-44 Activate Missed Approach; Key to activate the approach.; Figure 7-45 Descending Turn to the Initial Approach Fix (IAF)
  • Page 111 – After crossing FALUR the next waypoint is the; Figure 7-46 Descending to the FAF; After crossing CEGIX, the aircraft continues; Figure 7-47 Descending to the Missed Approach Point
  • Page 112 – SUSP; Figure 7-48 Missed Approach Active
  • Page 113 – Figure 7-49 Establishing the Holding Pattern; AIRPORT INFORMATION; Figure 7-53 Airport Information Page; Select the Airport Information Page
  • Page 114 – Select an Airport from the Active Flight Plan; Figure 7-54 Flight Plan Airport List; Select a Nearest Airport; Figure 7-55 Nearest Airport List; Select a Recently Entered Airport Identifier; Figure 7-56 Recently Entered Airports List
  • Page 115 – Access Runway Information; INTERSECTION INFORMATION; Select the Intersection Information Page; Figure 7-57 Intersection Information Page; Access Information on an Intersection
  • Page 116 – Figure 7-58 NDB Information Page; Select the NDB Information Page; View Information on a Specific NDB; Figure 7-59 VOR Information Page; Select the VOR Information Page; Access Information on a VOR
  • Page 117 – USER WAYPOINT INFORMATION; See the Flight Planning section for a discussion on; NEAREST AIRPORTS; Figure 7-60 Nearest Airports Page; Nearest Airport Information on the MFD; Select the Nearest Airports Page
  • Page 118 – Figure 7-61 Nearest Airports Window; NEAREST INTERSECTIONS; Figure 7-62 Nearest Intersections Page; Select the Nearest Intersections Page; View Information on the Nearest Intersection
  • Page 119 – Figure 7-63 Nearest NDB Page; Select the Nearest NDB Page; Access Information on a Specific NDB; Figure 7-64 Nearest VOR Page; Select the Nearest VOR Page; View Information on the Nearest VOR; Select and Load a VOR Frequency
  • Page 120 – NEAREST USER WAYPOINT; Figure 7-65 Nearest User Waypoints Page; Select the Nearest User Waypoint Page; Select a Nearest User Waypoint; Knob to activate the cursor.; NEAREST FREQUENCIES; Figure 7-66 Nearest Frequencies Page; Select the Nearest Frequencies Page; Select and Load the Nearest ARTCC, FSS, or
  • Page 121 – NEAREST AIRSPACES; Figure 7-67 Nearest Airspaces Page; Select the Nearest Airspaces Page; Airspace Alerts Box; • If the projected course takes the aircraft inside an; View Additional Details for a Listed Airspace; View and Quickly Load the Frequency for a
  • Page 123 – SECTION 8 – FLIGHT PLANNING; SECTION 8: FLIGHT PLANNING; The following discussions pertain to the Multi Function; USER DEFINED WAYPOINTS; Figure 8-1 User WPT Information Page; Select the User WPT Information Page; Create a New User Waypoint; Modify a User Waypoint; Delete a User Waypoint
  • Page 124 – VIEWING THE ACTIVE FLIGHT PLAN; Figure 8-2 Active Flight Plan Window on the PFD; ACTIVATE A STORED FLIGHT PLAN; Figure 8-4 Flight Plan Catalog Page; ob
  • Page 125 – ACTIVATE A FLIGHT PLAN LEG; Figure 8-5 Activate Flight Plan Leg Confirmation; STOP NAVIGATING A FLIGHT PLAN; Figure 8-6 Delete Flight Plan; INVERT ACTIVE FLIGHT PLAN; Key; Figure 8-8 Invert Flight Plan
  • Page 126 – CREATE A NEW FLIGHT PLAN; Create a New Flight Plan Using the MFD; Figure 8-10 Create FPL on MFD; Create a New Flight Plan Using the PFD; A flight plan cannot be entered using the; Figure 8-12 Creating Flight Plan on the PFD
  • Page 127 – ENTER AN AIRWAY IN A FLIGHT; FPL; Figure 8-13 Airway Insertion Point; Figure 8-14 Load Airway Entry Point; Figure 8-15 Airway Entry Point Loaded; Figure 8-16 Display Waypoint Information Window
  • Page 128 – LD AIRWY; Figure 8-17 Select Desired Airway; Figure 8-19 Airway Added to Flight Plan; LOAD A DEPARTURE
  • Page 129 – Figure 8-20 Store Flight Plan Confirmation; Figure 8-21 Remove Waypoint Confirmation
  • Page 130 – COPY A FLIGHT PLAN; DELETE A FLIGHT PLAN; GRAPHICAL FLIGHT PLAN CREATION; ABOVE; Figure 8-22 Trip Planning Page; Starting WPT
  • Page 131 – The Page Mode must be set to MANUAL
  • Page 133 – SECTION 9 – PROCEDURES; SECTION 9: PROCEDURES; ARRIVALS AND DEPARTURES; Load and Activate a Departure Procedure; Figure 9-1 Select Departure; Figure 9-2 Select Departure Transition; Load and Activate An Arrival Procedure; If any portion of an arrival procedure is
  • Page 134 – Knob to; to select the desired; Not all approaches in the database are approved for GPS; WAAS systems only
  • Page 135 – Figure 9-6 Selecting an Approach Procedure; Figure 9-7 Selecting an Approach Transition; Activate An Approach in the Active Flight Plan
  • Page 137 – SECTION 10: HAZARD AVOIDANCE; CUSTOMIZING THE HAZARD; Menu; Figure 10-1 Page Menu; Strike is less than 6 seconds old
  • Page 138 – At a map range of less than 25 nm, Stormscope; Figure 10-5 Lightning Display Range Annunciation; Stormscope Page; Figure 10-6 Stormscope Page; Cha
  • Page 139 – XM Weather is not intended to; MAP; Figure 10-7 Navigation Map Page Displaying NEXRAD Weather; WX; Figure 10-8 METAR and TAF Text Displayed on the
  • Page 140 – Figure 10-9 Weather Data Link Page; NEXRAD Limitations; Strikes depicted represent cloud to ground
  • Page 141 – Joystick; Weather Products and Symbols
  • Page 142 – Figure 10-10 Weather Product Symbols; The XM Information Page in the AUX Page Group will; The DONE Softkey on the AUX - XM; Weather Product Age; The age for each of the enabled products is displayed
  • Page 143 – Traffic Information Service (TIS) is only; Displaying Traffic on the Traffic Map Page; Figure 10-11 Traffic Map Page; Displaying Traffic on the Navigation Map; alert “Traffic” is given.
  • Page 144 – Refer to the Avidyne; Figure 10-12 Traffic Map Page
  • Page 145 – TERRAIN AND OBSTACLE PROXIMITY; Terrain data is not displayed when the; Figure 10-13 Obstacle Symbols; Color
  • Page 146 – Displaying Terrain on the TAWS Page
  • Page 147 – Red; Enable/Disable Aviation Data; While the TAWS Page is displayed, press the; MENU; Turn the small; Figure 10-17 TAWS Page Menu
  • Page 148 – TAWS System; OK; Reduced Required Terrain Clearance (RTC) and; Enroute
  • Page 149 – Figure 10-18 PDA Alerting; Negative Climb Rate After Takeoff; Don’t Sink
  • Page 150 – Figure 10-20 Negative Climb Rate; “Five-Hundred” Aural Alert; Potential Impact Points; Figure 10-21 TAWS Symbols; Displaying Terrain and Obstacles on the; With the Navigation Map displayed, press the; Press the; TERRAIN; Softkey. Terrain and obstacle
  • Page 151 – Alert Type
  • Page 152 – The following system status annunciations may also be; Alert Annunciations; Figure 10-23 Alert Annunciation on the TAWS Page; Alert Annunciation; Figure 10-24 Alert Annunciation on the PFD
  • Page 153 – SECTION 11: ABNORMAL; REVERSIONARY MODE; Should a system detected failure occur in either display,; Normal PFD Display; Reversionary display mode can also be manually; The Diamond DA40 Airplane Flight Manual
  • Page 154 – Figure 11-2 Extreme Pitch Indication
  • Page 155 – Dead Reckoning Mode will only function in; Symbolic Aircraft
  • Page 157 – SECTION 12 – ANNUNCIATIONS
  • Page 158 – ALERT LEVEL DEFINITIONS
  • Page 159 – AIRCRAFT ALERTS; The following alerts are configured specifically for; WARNING Alerts; L FUEL LOW; Message Advisory Alerts; PFD FAN FAIL
  • Page 160 – The following alert annunciations appear in the AFCS; Condition; If; Figure 12-5 AFCS System Status Annunciation; System Status Annunciation
  • Page 162 – When an LRU or an LRU function fails, a large red
  • Page 163 – System Annunciation
  • Page 164 – Figure 12-6 G1000 System Failure Annunciations; Aural Alert; “Vertical track”
  • Page 168 – Message
  • Page 172 – TRUE APR
  • Page 179 – INDEX; Signal augmentation 5-2
  • Page 180 – Load the nearest ARTCC frequency
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Cockpit Reference Guide

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DA40/40F

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Summary

Page 9 - RECORD OF REVISIONS; Part Number

Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A RECORD OF REVISIONS RR-1 Part Number Change Summary 190-00324-00 Initial Release 190-00324-01 Reformat of manualAdded NAV/COM volume levelsAdded Flight TimerAdded extended range fuel tanksChanged NAV1 and NAV2 on the PFD to VO...

Page 10 - Revision Date of Revision Affected Pages

Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A RECORD OF REVISIONS RR-2 Revision Date of Revision Affected Pages Description A 5/07 i-Index-4 Production Release

Page 11 - TABLE OF CONTENTS; Section 1: System Overview

Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A i TABLE OF CONTENTS Section 1: System Overview ......................................... 1-1 1.1 PFD/MFD Controls ................................................... 1-2 1.2 PFD Softkeys ..........................................

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