Garmin DA40F- User Manual

Garmin DA40F

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Table of Contents:

  • Page 7 – RECORD OF REVISIONS; Part Number
  • Page 8 – Blank Page
  • Page 9 – TABLE OF CONTENTS; SECTION 1: SYSTEM OVERVIEW
  • Page 10 – ii; SECTION 7: NAVIGATION
  • Page 11 – iii; SECTION 9: PROCEDURES
  • Page 12 – iv; INDEX
  • Page 13 – The purpose of this Cockpit Reference Guide is to; The pilot should read and thoroughly
  • Page 14 – MFD Only
  • Page 16 – Softkey OFF
  • Page 17 – Figure 1-3 PFD Softkey Flow Chart – 1; Figure 1-4 PFD Softkey Flow Chart – 2; BRG2 (bearing) – Press to cycle through the
  • Page 18 – METRIC; Figure 1-5 PFD Softkey Flow Chart – 3; OBS
  • Page 19 – Figure 1-6 MFD Softkeys
  • Page 20 – Figure 1-7 Page Group Icon
  • Page 21 – FMS; Figure 1-8 PFD Setup Menu Window; XM Radio audio will be automatically muted when the; DATABASE UPDATES; Aviation Database Update; The display downloads the aviation; ENT; Figure 1-10 Database Update Confirmation; Terrain and Obstacle Database Updates; The data contained in the terrain and
  • Page 22 – These databases are not stored internally in the MFD; If the Supplemental Data Card is; TOPO; and; RAIN; softkeys are not functional and are grayed; Figure 1-11 Power-Up Splash Screen Window
  • Page 23 – SECTION 2: FLIGHT INSTRUMENTS; Figure 2-1 Default PFD Information
  • Page 24 – Figure 2-2 Additional PFD Information; Next Waypoint
  • Page 25 – 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 26 – Figure 2-7 Altimeter; Altitude Select Bug; Set the Selected Altitude Bug:; Turn the; Knobs to set the Altitude Select; ALT; Knob sets the hundreds and; ALT; Knob sets the thousands. This; Altitude Trend Vector; BARO; Altitude Alerting; Figure 2-8 Altitude Alerting Visual Annunciations; Barometric Minimum Descent Altitude
  • Page 27 – Figure 2-9 Barometric Minimum Descent Altitude; MARKER BEACON ANNUNCIATIONS; Figure 2-10 Marker Beacon and Vertical Deviation; INDICATOR; Figure 2-11 Vertical Speed Indicator; VS; HORIZONTAL SITUATION INDICATOR; PFD
  • Page 28 – Figure 2-14 Standard-Rate Turn Indication; Course Pointer; Figure 2-15 Arc CDI and Compass Rose CDI
  • Page 29 – Figure 2-16 HSI with Bearing Information; Figure 2-19 DME Information Window; Navigation Source; Change between navigation sources:; Softkey to change from GPS to; Softkey again to change from; CDI; Softkey a third time to return to
  • Page 30 – When using GPS as the navigation source, the following; Softkey to select OBS Mode.; CRS; Knob to select the desired course; Softkey again to return to; The; Softkey is only displayed when
  • Page 31 – SECTION 3 – ENGINE; SECTION 3: ENGINE INDICATION; ENGINE; Figure 3-1 DA40 Default Engine Display; Green; Figure 3-3 Fuel Pressure Indicator
  • Page 32 – LEAN ENGINE DISPLAY; Cylinder Select; CYL SLCT; Figure 3-4 DA40 LEAN Engine Display; ASSIST
  • Page 33 – ENGINE SYSTEM DISPLAY; If desired, use the; Fuel calculations do not use the aircraft
  • Page 35 – TRANSPONDER; The NAV/COM controls and frequency boxes are
  • Page 36 – Figure 4-2 Frequency Fields
  • Page 37 – RADIO STATUS INDICATIONS; Figure 4-5 Radio Status Indications; AUTOMATIC SQUELCH; COM; OPTIONAL NAV RADIOS; DME
  • Page 38 – Figure 4-9 DME Selection Window; Auto-tuning on the PFD
  • Page 39 – STBY; Figure 4-11 Ground Mode; Reply Status; Figure 4-12 Reply Indication; Code Selection; Flight ID Reporting
  • Page 41 – SECTION 5 – AUDIO PANEL; SECTION 5: AUDIO PANEL; Figure 5-1 Audio Panel Controls
  • Page 42 – 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 43 – PILOT; Figure 5-6 ICS Isolation; INTERCOM SQUELCH CONTROL; MAN SQ
  • Page 44 – DIGITAL CLEARANCE RECORDER; PLAY
  • Page 45 – SECTION 6: AUTOMATIC FLIGHT; Figure 6-1 AFCS Keys; MODE ANNUNCIATIONS
  • Page 46 – Figure 6-3 PFD AFCS Display; OVERSPEED PROTECTION; Figure 6-4 Overspeed Annunciation; AP; Figure 6-5 Autopilot Engaged Annunciation
  • Page 47 – Figure 6-6 Automatic Disconnect Annunciation; Automatic Disconnect; Manual Disengagement; Figure 6-7 Manual Disconnect Annunciation; Manual Disconnect; Figure 6-8 CWS Annunciation; Control Wheel Steering; Figure 6-9 Loss of VOR Signal; PITCH AXIS MODES; AFCS Key
  • Page 48 – Figure 6-10 Pitch Hold Mode; CWS
  • Page 49 – Figure 6-11 Altitude Hold Mode; If the Selected Altitude is captured during; button after the Selected Altitude is
  • Page 50 – Figure 6-12 Vertical Speed Hold Mode
  • Page 51 – toward; FLC; Figure 6-13 Flight Level Change Mode
  • Page 52 – GA; Pressing the CWS button while Glideslope; APR
  • Page 53 – Mode annunciations for active roll axis modes are; Figure 6-15 Roll Hold Mode
  • Page 54 – Figure 6-16 Heading Select Mode; HDG
  • Page 55 – NAV; When making a backcourse approach, set; Navigation Mode Armed
  • Page 56 – The Approach mode acquires and tracks the selected; While using Approach mode, the; See the Example Procedures Using AFCS section for
  • Page 57 – EXAMPLE PROCEDURES USING AFCS; This section provides a scenario-based set of procedures; Figure 6-19 Flight Plan Overview
  • Page 58 – Figure 6-20 Departure
  • Page 59 – Changing the HSI mode cancels; Figure 6-21 Intercepting a VOR
  • Page 60 – Figure 6-22 Transition to GPS Flight Plan
  • Page 61 – While flying the GPS leg from Panoche VORTAC to; Knob, set the Selected Altitude; Key to activate Flight Level; Figure 6-23 FLC Descent; ) Reduce power to allow descent in Flight Level
  • Page 62 – Figure 6-24 ILS Approach to KFAT
  • Page 63 – Flashes for five seconds
  • Page 65 – SECTION 7 – NAVIGATION; The following discussions pertain to the Multi Function; NAVIGATION MAP PAGE; Select the MAP Page Group; The map display should only be; Direct-to Navigation from the MFD
  • Page 66 – Figure 7-3 Canceling Direct-to Navigation; Direct-to Navigation from the PFD
  • Page 67 – AIRPORT INFORMATION; Figure 7-5 Airport Information Page; Select the Airport Information Page
  • Page 68 – INTERSECTION INFORMATION; Select the Intersection Information Page; Figure 7-6 Intersection Information Page; Select the NDB Information Page
  • Page 69 – Figure 7-8 VOR Information Page; Select the VOR Information Page; USER WAYPOINT INFORMATION; See the Flight Planning section for a discussion on; NEAREST AIRPORTS; Figure 7-9 Nearest Airports Page; Nearest Airport Information on the MFD
  • Page 70 – Figure 7-10 Nearest Airports Window
  • Page 71 – NEAREST INTERSECTIONS; Figure 7-11 Nearest Intersections Page; Select the Nearest Intersections Page; Figure 7-12 Nearest NDB Page; Select the Nearest NDB Page
  • Page 72 – Figure 7-13 Nearest VOR Page; NEAREST USER WAYPOINT; Figure 7-14 Nearest User Waypoints Page; Select the Nearest User Waypoint Page
  • Page 73 – NEAREST FREQUENCIES; Figure 7-15 Nearest Frequencies Page; Select the Nearest Frequencies Page; NEAREST AIRSPACES; Figure 7-16 Nearest Airspaces Page; Select the Nearest Airspaces Page; • If the projected course takes the aircraft inside an
  • Page 75 – SECTION 8 – FLIGHT PLANNING; SECTION 8: FLIGHT PLANNING; USER DEFINED WAYPOINTS; Figure 8-1 User WPT Information Page; Select the User WPT Information Page
  • Page 76 – 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
  • Page 77 – 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; Figure 8-8 Invert Flight Plan; CREATE A NEW FLIGHT PLAN; Create a New Flight Plan Using the MFD
  • Page 78 – Figure 8-10 Create FPL on MFD; Create a New Flight Plan Using the PFD; A flight plan cannot be entered using the; LOAD A DEPARTURE; See the Procedures section for a discussion on loading
  • Page 79 – Figure 8-13 Store Flight Plan Confirmation
  • Page 80 – INVERT AND ACTIVATE A STORED
  • Page 81 – Figure 8-15 Trip Planning Page; Starting WPT; The Page Mode must be set to MANUAL
  • Page 82 – : An active flight plan or Direct-to must be; NOTE; : VNAV is advisory only and cannot be; Create a Vertical Navigation Profile
  • Page 83 – Key. The cursor is now placed; MAP; VNAV Page Menu Options; MENU
  • Page 85 – SECTION 9 – PROCEDURES; ARRIVALS AND DEPARTURES; Load and Activate a Departure Procedure; Figure 9-1 Select Departure; Load and Activate an Arrival Procedure; Figure 9-3 Select Arrival
  • Page 86 – Figure 9-4 Select Arrival Transition; Not all approaches in the database are approved for GPS; Load and/or Activate an Approach Procedure; Figure 9-6 Selecting an Approach Procedure
  • Page 87 – Figure 9-7 Selecting an Approach Transition; Activate An Approach in the Active Flight Plan
  • Page 89 – SECTION 10: HAZARD AVOIDANCE; CUSTOMIZING THE HAZARD; Figure 10-1 Page Menu
  • Page 90 – Figure 10-5 METAR and TAF Text Displayed on the; NEXRAD
  • Page 91 – Strikes depicted represent cloud to ground; to display the panning; Joystick; to place the panning arrow; Key to display pertinent information
  • Page 92 – Note that pressing the; Key when panning; Key and; Key; Weather Products and Symbols; Figure 10-7 depicts the symbol for each weather; Figure 10-7 Weather Product Symbols; Echo Top (Cloud Top and Echo Top Mutually Exclusive); The DONE Softkey on the AUX - XM; Weather Product Age; The age for each of the enabled products is displayed
  • Page 93 – Weather Product; Traffic Information Service (TIS) is only; Displaying Traffic on the Traffic Map Page; If data is not received for a period longer than 6 seconds,
  • Page 94 – Figure 10-8 Traffic Map Page; Displaying Traffic on the Navigation Map; alert “Traffic” is given.; TERRAIN AND OBSTACLE PROXIMITY; Terrain data is not displayed when the
  • Page 95 – Color; Figure 10-11 Obstacle Symbols; ) With the Navigation Map displayed, press the; Softkey. Terrain and obstacle; Figure 10-10 Topography Scale
  • Page 96 – Displaying Terrain on the TAWS Page
  • Page 97 – Black; Enable/Disable Aviation Data; Figure 10-14 TAWS Page Menu; TAWS Inhibit; Flying VFR into an area where unique terrain exists
  • Page 98 – TAWS System; ) While the TAWS Page is displayed, press the; Enroute; Figure 10-15 PDA Alerting
  • Page 99 – Figure 10-16 Excessive Descent Rate; Negative Climb Rate After Takeoff; Don’t Sink; Figure 10-17 TAWS Symbols; “Five-Hundred” Aural Alert
  • Page 100 – When the Navigation Map Page is displayed, and a
  • Page 101 – Alert Type
  • Page 102 – The following system status annunciations may also be; Alert Annunciations; Figure 10-19 Alert Annunciation on the TAWS Page; Alert Annunciation; Figure 10-20 Alert Annunciation on the PFD
  • Page 103 – 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 104 – ABNORMAL COM OPERATION; When a COM tuning failure is detected by the system,; UNUSUAL ATTITUDES; The PFD will ‘declutter’ when the aircraft enters an; Figure 11-2 Extreme Pitch Indication; HAZARD DISPLAYS WITH LOSS OF; If GPS position is lost, or becomes invalid, selected; Figure 11-3 Loss of Hazard Functions
  • Page 105 – SECTION 12 – ANNUNCIATIONS; ALERTS
  • Page 106 – ALERT LEVEL DEFINITIONS
  • Page 107 – AIRCRAFT ALERTS; The following alerts are configured specifically for; WARNING Alerts; L FUEL LOW; Message Advisory Alerts; PFD FAN FAIL
  • Page 108 – The following alert annunciations appear in the AFCS; Condition; If; Figure 12-5 AFCS System Status Annunciation; System Status Annunciation
  • Page 110 – When an LRU or an LRU function fails, a large red
  • Page 111 – System Annunciation
  • Page 112 – Figure 12-6 G1000 System Failure Annunciations
  • Page 113 – Message
  • Page 114 – Alerts Window Message
  • Page 117 – GEA 71 Message Advisories
  • Page 118 – GRS 77 Message Advisories
  • Page 121 – SLCT AUTOSEQ
  • Page 123 – Signal augmentation 5-2
  • Page 124 – Military interceptor operations code
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Integrated Flight Deck

Cockpit Reference Guide

Diamond

DA40/40F

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Summary

Page 7 - RECORD OF REVISIONS; Part Number

Garmin G1000 Cockpit Reference Guide for the DA40/40F 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 VOR or LOCMoved altitu...

Page 8 - Blank Page

Garmin G1000 Cockpit Reference Guide for the DA40/40F RECORD OF REVISIONS RR-2 Blank Page

Page 9 - TABLE OF CONTENTS; SECTION 1: SYSTEM OVERVIEW

Garmin G1000 Cockpit Reference Guide for the DA40/40F i TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW .................................... 1-1 1.1 PFD/MFD Controls ................................................... 1-2 1.2 PFD Softkeys ............................................................ 1-4...

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