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 ..........................................
Page 12 - ii; Section 7: Navigation
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A ii TABLE OF CONTENTS Approach .................................................................. 6-30Go Around/Missed Approach ..................................... 6-32 6.6 AFCS Annunciations and Alerts .........................
Page 13 - iii; Section 11: Abnormal Operation
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A iii TABLE OF CONTENTS 10.4 Traffic Information Service (TIS) ....................... 10-7 Displaying Traffic on the Traffic Map Page ................... 10-7Displaying Traffic on the Navigation Map ................... 10-7TIS Audi...
Page 14 - iv; Blank Page
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A iv TABLE OF CONTENTS Blank Page
Page 15 - SECTION 1: SYSTEM OVERVIEW; The purpose of this Cockpit Reference Guide is to; The pilot should read and thoroughly
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 1-1 SECTION 1 SYSTEM OVERVIEW 1-1 SECTION 1: SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system mor...
Page 16 - MFD Only
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 1-2 SECTION 1 SYSTEM OVERVIEW 1.1 PFD/MFD CONTROLS Figure 1-1 PFD/MFD Controls 4 2 1 6 5 7 9 8 3 12 13 11 10 16 15 14 MFD Only (with optional GFC 700) 17 27 26 25 28 18 19 23 22 21 20 24
Page 19 - Softkey OFF; Figure 1-3 INSET Softkeys; INSET
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 1-5 SECTION 1 SYSTEM OVERVIEW 1.2 PFD SOFTKEYS Softkey OFF Softkey ON Figure 1-2 PFD Top Level Softkeys ADF/DME Press the BACK or OFF Softkey to return to the top-level softkeys. ALERTS STRMSCP ALERTS ADF/DME Figure 1-3 INSET ...
Page 20 - Figure 1-4 PFD Configuration Softkeys; PFD
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 1-6 SECTION 1 SYSTEM OVERVIEW Figure 1-4 PFD Configuration Softkeys Press the STD BARO or BACK Softkey to return to the top-level softkeys BRG1 (NAV1) BRG1 (GPS) BRG1 (OFF) DME ALT UNIT METERS IN HPA ALERTS ALERTS ALERTS ALERTS...
Page 21 - OBS; XPDR
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 1-7 SECTION 1 SYSTEM OVERVIEW GPS – Displays GPS waypoint identifier and GPS distance information in the BRG2 Information Window. ADF – Displays ADF in the BRG2 Information Window. O F F – R e m o v e s t h e B R G 2 I n f o r ...
Page 22 - Figure 1-6 MFD Softkeys
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 1-8 SECTION 1 SYSTEM OVERVIEW IDENT – Press to provide special aircraft position identification to Air Traffic Control (ATC). TMR/REF – Press to display the Timer/References Window. NRST – Press to display the Nearest Airports W...
Page 23 - Figure 1-7 Page Group Icon; Turn the large; Knob; FMS; Knob; to select pages within the
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 1-9 SECTION 1 SYSTEM OVERVIEW STRMSCP (optional) – Pressing this softkey displays/ removes Stormscope lightning data on the Navigation Map. NEXRAD (optional) – Pressing this softkey displays/ removes precipitation data on the ...
Page 24 - VERTICAL NAVIGATION; All arrival procedure altitudes contained in
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 1-10 SECTION 1 SYSTEM OVERVIEW 1.5 VERTICAL NAVIGATION In WAAS capable installations, one of two altitude sources is used by the G1000 when giving vertical navigation guidance. WAAS GPS altitude is used when giving guidance fo...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 1-11 SECTION 1 SYSTEM OVERVIEW White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the system estimating the altitude of the aircraft as it passes over the navigation point. This altitude is pr...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 1-12 SECTION 1 SYSTEM OVERVIEW 1.6 BACKLIGHTING When system power is turned off, all manual backlighting settings will return to the factory default settings. Manually adjust the backlight for the PFD and MFD: 1) Press the MEN...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 1-13 SECTION 1 SYSTEM OVERVIEW 3) Press the ENT Key to start the database update. A prompt similar to the following is displayed: Figure 1-12 Database Update Confirmation 4) After the update completes, the PFD starts in normal ...
Page 29 - SECTION 2: FLIGHT INSTRUMENTS; Figure 2-1 Default PFD Information
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 2-1 SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated. 6 7 11 14 15 8 13 12 5 3 4 2 1 16 Figure 2-1 Default PFD Information 1...
Page 30 - Figure 2-2 Additional PFD Information; Flight Plan Messages/Indications
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 2-2 SECTION 2 FLIGHT INSTRUMENTS Figure 2-2 Additional PFD Information 2 1 5 3 4 8 6 Traffic Annunciation 2 4 3 1 Selected Heading Box 9 Flight Plan Window 10 Barometric Minimums Box 8 BRG2 Information Window Vspeed References ...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 2-3 SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Figure 2-4 Airspeed Indicator Actual Airspeed Airspeed Trend Vector True Airspeed Box Speed Ranges (low end yellow band not displayed and other low end speed ranges diffe...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 2-4 SECTION 2 FLIGHT INSTRUMENTS 2.3 ALTIMETER Altitude Reference Box Altitude Trend Vector Current Altitude Barometric Setting Box Altitude Reference Bug Figure 2-7 Altimeter Barometric Altitude Minimums Bug Selected Altitude...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 2-5 SECTION 2 FLIGHT INSTRUMENTS Metric Display Display altitude in meters and barometric pressure in hectopascals: 1) Press the PFD Softkey to display the second level softkeys. 2) Press the ALT UNIT Softkey. 3) Press the MET...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 2-6 SECTION 2 FLIGHT INSTRUMENTS 2.4 VERTICAL DEVIATION/GLIDEPATH/ GLIDESLOPE INDICATOR The Vertical Deviation and Required Vertical Speed Indicators appear when vertical guidance is being given prior to executing an approach ...
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:
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 2-7 SECTION 2 FLIGHT INSTRUMENTS 2.5 MARKER BEACON ANNUNCIATIONS Figure 2-14 Marker Beacon Annunciations Outer Marker Middle Marker Inner Marker Altimeter 2.6 VERTICAL SPEED INDICATOR Figure 2-15 Vertical Speed Indicator Verti...
Page 36 - Altitude Reached; Figure 2-17 Barometric Minimum Descent Altitude; Barometric; HORIZONTAL SITUATION INDICATOR
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 2-8 SECTION 2 FLIGHT INSTRUMENTS Alerting is inhibited while the aircraft is on the ground. If the aircraft climbs after having reached the MDA, once it reaches 50 feet above the MDA, alerting is disabled. Within 100 ft Altitu...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 2-9 SECTION 2 FLIGHT INSTRUMENTS Turn Rate Indicator and Heading Trend Vector Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta turn rate trend vector shows the current...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 2-10 SECTION 2 FLIGHT INSTRUMENTS 2.0 nm Enroute (Oceanic if >200 nm from nearest airport) 0.3 nm Missed Approach 1.0 nm Approach 1.0 nm Terminal 1.0 nm Terminal 0.3 nm Departure CDI Full-scale Deflection 31 nm from Destina...
Page 39 - Figure 2-25 HSI with Bearing Information; Figure 2-28 DME Information Window; Navigation Source; Change CDI navigation sources:; CDI
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 2-11 SECTION 2 FLIGHT INSTRUMENTS Bearing Pointers and Information Windows Pressing the PFD Softkey provides access to the BRG1 and BRG2 Softkeys. The BRG1 pointer is a single line pointer. The BRG2 pointer is a double line po...
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:
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 2-12 SECTION 2 FLIGHT INSTRUMENTS • SUSP – Displayed when in OBS Mode indicating GPS waypoint sequencing is suspended. • DR – Navigating using Dead Reckoning due to an error in the GPS solution. Figure 2-29 GPS LOI, GPS SUSP, ...
Page 41 - Figure 2-31 Timer Status Prompts; Change the Generic Timer:
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 2-13 SECTION 2 FLIGHT INSTRUMENTS 2.10 GENERIC TIMER Figure 2-31 Timer Status Prompts Change the Generic Timer: 1) Press the TMR/REF Softkey, then turn the large FMS Knob to select the time field (hh/mm/ss). Turn the FMS Knobs ...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-1 SECTION 3: ENGINE INDICATION SYSTEM (EIS) The Engine Instrument Display is displayed on the left side of the MFD. DA40F DA40 Figure 3-1 Engine Instrument Display on the MFD Manifo...
Page 44 - ENGINE; Fuel Totalizer; DEC FUEL
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-2 3.1 DA40 ENGINE DISPLAY Pressing the ENGINE Softkey displays the EIS- ENGINE Page as shown in Figure 3-2. Fuel used (GALLONS USED), endurance, and range (RANGE NM) are all calcula...
Page 46 - LEAN
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-4 3.3 ENGINE LEANING While viewing the EIS-ENGINE Page, press the LEAN Softkey. As the mixture is leaned, one of the cylinder’s exhaust temperature will peak. This is indicated by ‘...
Page 49 - TRANSPONDER; The NAV/COM controls and frequency boxes are
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 4-1 SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER The NAV/COM controls and frequency boxes are located on the Primary Flight Display and the Multi Function Display in the same locations. NAV Controls...
Page 50 - Figure 4-2 Frequency Fields
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 4-2 SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Active NAV Frequency Field Active COM Frequency Field Standby COM Frequency Field Figure 4-2 Frequency Fields Selected NAV Frequency Tuning Box Tuning Box S...
Page 51 - RADIO STATUS INDICATIONS; Figure 4-5 Radio Status Indications; AUTOMATIC SQUELCH; COM; OPTIONAL NAV RADIOS; DME
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 4-3 SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception. • TX – When a COM radio is transmitting, a ...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 4-4 SECTION 4 – NAV/COM & TRANSPONDER DME Radio (optional) Figure 4-8 ADF/DME Tuning Window Change the DME tuning source: 1) From the tuning window, turn the large FMS Knob to highlight the desired DME source. 2) Turn the ...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 4-5 SECTION 4 – NAV/COM & TRANSPONDER Standby Mode (Manual) Press the STBY Softkey. In Standby Mode, the tran- sponder does not reply to interrogations, but new codes can be entered. STBY Mode (White Code Number and Mode) ...
Page 54 - Enter Code Using the FMS Knob; Flight ID Reporting; If so configured, the Flight ID may be entered in the
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 4-6 SECTION 4 – NAV/COM & TRANSPONDER Enter Code Using the FMS Knob 1) Press the XPDR Softkey to display the transponder Mode Selection softkeys. 2) Press the CODE Softkey to display the transponder Code Selection softkeys...
Page 55 - SECTION 5 – AUDIO PANEL; SECTION 5: AUDIO PANEL; Figure 5-1 Audio Panel Controls
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 5-1 SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transmitters (COM3 MIC is unavailable) Transceiver Audio (COM 3 is unavailable) Split COM (Unavailable) Telephone (Unavailable) Marker Beacon/Mute Passenger Address Marker Bea...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 5-2 SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Pressing the COM1 MIC or COM2 MIC Key selects the active transmitter (i.e., microphone). The associated receiver audio ( COM1 or COM2 ) also becomes selected when the COM MIC...
Page 57 - PILOT; Figure 5-6 ICS Isolation; INTERCOM SQUELCH CONTROL; MAN SQ
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 5-3 SECTION 5 – AUDIO PANEL 5.4 INTERCOM SYSTEM (ICS) ISOLATION Press the PILOT and/or COPLT Key to select who is isolated from hearing the NAV/COM radios and music. Selection scenarios are addressed in Table 5-1. Figure 5-6 I...
Page 58 - DIGITAL CLEARANCE RECORDER; PLAY
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 5-4 SECTION 5 – AUDIO PANEL 5.6 DIGITAL CLEARANCE RECORDER AND PLAYER Each reception of primary active COM audio is automatically recorded in a memory block. When the next transmission is received, it is recorded in the next m...
Page 59 - SECTION 6: AUTOMATIC FLIGHT; Figure 6-1 AFCS Keys; AP DISC (Autopilot Disconnect) Button; FLIGHT DIRECTOR OPERATION
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-1 SECTION 6: AUTOMATIC FLIGHT CONTROL The GFC 700 AFCS is optional on the DA40 and DA40F. In aircraft without the GFC 700 option, refer to the operating instructions for the installed aut...
Page 60 - FD; Figure 6-2 PFD AFCS Display; Command Bars; Figure 6-3 Command Bars
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-2 Activating the Flight Director Pressing the FD or AP Key (when the flight director is not active) activates the flight director in default pitch/roll modes. Pushing the GA Switch or any fl...
Page 61 - FLIGHT DIRECTOR MODES; Figure 6-4 Loss of VOR Signal; Pitch Modes
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-3 AFCS Status Box Flight director roll modes are shown on the left and pitch on the right. Armed modes are annunciated in white and active in green. Autopilot status is displayed in the c...
Page 62 - Table 6-1 lists the pitch modes with their corresponding; ALTS; Table 6-1 Flight Director Pitch Modes
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-4 Table 6-1 lists the pitch modes with their corresponding controls and annunciations. The mode reference (shown with default measurement units) is displayed next to the active mode annun...
Page 63 - Figure 6-5 Pitch Hold Mode; Changing the Pitch Reference
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-5 Pitch Hold Mode (PIT) When the flight director is activated (the FD Key is pressed), Pitch Hold Mode is selected by default. Pitch Hold Mode is indicated as the active pitch mode by the ...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-6 Selected Altitude Capture Mode (ALTS) Selected Altitude Capture Mode arms automatically when the flight director is in Pitch Hold, Vertical Speed, Flight Level Change, or Go Around Mode....
Page 65 - If the Selected Altitude is reached during CWS; Figure 6-7 Altitude Hold Mode; In Vertical Speed Mode, the flight director acquires
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-7 If the Selected Altitude is reached during CWS maneuvering, the Altitude Reference is not changed. To adjust the Altitude Reference in this case, the CWS Button must be pressed again af...
Page 66 - Figure 6-8 Vertical Speed Mode; Changing the Vertical Speed Reference; The Selected Altitude should be set before; FLC
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-8 Figure 6-8 Vertical Speed Mode Vertical Speed Reference Bug Selected Altitude Command Bars Indicate Climb to Attain Vertical Speed Vertical Speed Mode Active Vertical Speed Reference Se...
Page 67 - Changing the Airspeed Reference; Figure 6-9 Flight Level Change Mode
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-9 descent). The flight director maintains the current altitude until either engine power or the Airspeed Reference are adjusted and does not allow the aircraft to climb or descend away fro...
Page 68 - Figure 6-10 Vertical Path Tracking Armed Annunciations; VNV
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-10 Vertical Navigation Modes (VPTH, ALTV) NOTE: Pressing the CWS Button while Vertical Path Tracking Mode is active does not cancel the mode. The autopilot guides the aircraft back to the...
Page 69 - In conjunction with the “TOD [top of descent] within 1; Figure 6-11 Vertical Path Capture
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-11 In conjunction with the “TOD [top of descent] within 1 minute” annunciation in the Navigation Data Box, VNAV indications (VNAV Target Altitude, vertical deviation, and vertical speed r...
Page 70 - Figure 6-12 Vertical Path Tracking Mode; Automatic Pitch Hold Reversion
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-12 When a descent leg is captured (Figure 6-12), Vertical Path Tracking becomes active and tracks the descent pro-file. An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed as appropriate....
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-13 VNAV flight control is selected. If the VS or FLC Key is pressed while Vertical Path Tracking Mode is selected, Vertical Path Tracking Mode reverts to armed along with the appropriate a...
Page 72 - Button while Glidepath; Figure 6-15 Glidepath Mode; APR
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-14 Changing the current VNAV Target Altitude while VNAV Target Altitude Capture Mode is active causes the flight director to revert to Pitch Hold Mode. Vertical Path Tracking and the appro...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-15 Figure 6-16 Glidepath Mode Armed If vertical guidance becomes or is expected to become unavailable and the approach downgrades, Glidepath Mode is disarmed. When vertical guidance becom...
Page 74 - Figure 6-19 Go Around Mode; Roll Modes
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-16 Go Around (GA) Mode Pushing the GA Switch engages the flight director in a wings level, 7° pitch-up attitude, allowing the execution of a missed approach or a go around. This mode is a ...
Page 75 - If Roll Hold Mode is activated as a result; Changing the Roll Reference
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-17 Table 6-2 relates each roll mode to its respective control and annunciation. Refer to the pitch modes section for information regarding Go Around Mode. The CWS Button does not change l...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-18 Heading Select Mode (HDG) Heading Select Mode is activated by pressing HDG Key. Heading Select Mode acquires and maintains the Selected Heading. The Selected Heading is shown by a ligh...
Page 77 - The selected navigation receiver must have; Figure 6-22 Navigation Mode; Course and deviation.; NAV; Figure 6-23 GPS Navigation Mode Armed
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-19 Navigation Mode (GPS, VOR, LOC, BC) NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the flight director to enter Navigation Mode. Pre...
Page 78 - Changing the Selected Course
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-20 When the CDI has automatically switched from GPS to LOC during a LOC/ILS approach, GPS Navigation Mode remains active, providing GPS steering guidance until the localizer signal is cap...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-21 6.4 AUTOPILOT OPERATION NOTE: Refer to the AFM for specific instructions regarding emergency procedures. The autopilot operates flight control surface servos to provide automatic flight c...
Page 80 - Figure 6-27 Automatic Autopilot Disengagement; Autopilot Automatically Disengaged; Figure 6-28 Manual Autopilot Disengagement; Autopilot Manually Disengaged
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-22 Disengaging the Autopilot Automatic disengagement occurs due to: • System failure• Inability to compute default flight director modes (FD also disengages automatically) • Invalid sensor...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-23 6.5 EXAMPLE PROCEDURES USING AFCS NOTE: The diagrams in this section are for instruc- tional purposes only and should not be used for navigation. This section provides a scenario-based...
Page 82 - Figure 6-30 Departure
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-24 Departure Climbing to the Selected Altitude and flying an assigned heading:1) Before takeoff, set the Selected Altitude to 12,000 feet using the ALT Knob. 2) In this example, Vertical S...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-25 Intercepting a VOR Radial During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Airway V4 to Salina VOR (SLN) should now be intercepted. Since the enrout...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-26 Flying a Flight Plan/GPS Course NOTE: Changing the navigation source cancels Navigation Mode and causes the flight director to revert back to Roll Hold Mode (wings rolled level). As the...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-27 Descent While flying the arrival procedure, the aircraft is cleared for descent in preparation for the approach to KCOS. Three methods are presented for the descent from 12,000 ft: • Fl...
Page 86 - Figure 6-34 VPTH Descent
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-28 Vertical Path Tracking descent to VNV Target Altitude: 1) Select coupled VNAV: a) Press the VNV Key to arm Vertical Path Tracking Mode. The white annunciation ‘VPTH’ appears. b) Using ...
Page 87 - Knob, set the Selected Altitude; Key before the planned TOD
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-29 Non-path descent using Flight Level Change Mode: 1) Command a non-path descent using Flight Level Change Mode: a) Using the ALT Knob, set the Selected Altitude below the current aircra...
Page 88 - Flying an ILS approach:; KCOS; Figure 6-36 ILS Approach to KCOS
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-30 Approach Flying an ILS approach: 1) Transition from GPS Navigation Mode to Heading Select Mode. a) Select the Runway 35L ILS approach for KCOS and select ‘VECTORS’ for the transition. ...
Page 89 - Flying a WAAS precision approach:; Figure 6-37 LPV Approach to KCOS
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-31 Flying a WAAS precision approach: 1) A r m f l i g h t d i r e c t o r m o d e s f o r a p r e c i s i o n approach: a) Make sure the navigation source is set to GPS (use CDI Softkey t...
Page 90 - Flying a missed approach:; Flashes 5 sec; As a result of calculations performed by
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-32 Go Around/Missed Approach Flying a missed approach: 1) Push the GA Switch at the Decision height and apply full power to execute a missed approach. The flight director Command Bars esta...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-33 6.6 AFCS ANNUNCIATIONS AND ALERTS AFCS Status Alerts The following annunciations (listed in order of increasing priority) can appear on the PFD above the Airspeed and Attitude indicato...
Page 92 - Overspeed protection is provided in situations where; Figure 6-40 Overspeed Annunciation; Airspeed
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-34 Overspeed Protection Overspeed protection is provided in situations where the flight director cannot acquire and maintain the vertical Mode Reference for the selected vertical mode with...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-1 SECTION 7: NAVIGATION The majority of the following discussions pertain to the Multi Function Display. In discussions pertaining to the PFD, the controls are located on the PFD. 7.1 NAVIGATION MAP PA...
Page 95 - Manually Define the Active Direct-to; Figure 7-6 Canceling Direct-to Navigation; Direct-to Navigation from the PFD
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-3 Figure 7-5 Recently Entered Waypoints List (MFD) 3) Turn the small FMS Knob to the right to display the ‘RECENT’ waypoints as shown in Figure 7-5. 4) Turn the large FMS Knob to select the desired air...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-5 3) Turn the small FMS Knob to the right to display the ‘NRST’ airports to the aircraft’s current position as shown in Figure 7-9. 4) Turn the large FMS Knob to select the desired airport. 5) Press th...
Page 99 - Figure 7-13 Begin Adding V4 to the Flight Plan
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-7 4) V4 will now be entered into the flight plan. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to highlight the desired entry point as shown in Figure 7-13. The V4 entry will...
Page 100 - Figure 7-16 List of Available Airways for TOP
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-8 f) Press the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 7-16. Figure 7-16 List of Available Airways for TOP g) Turn either FMS Knob to highlight V4 in the lis...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-9 Figure 7-19 V4 is Loaded in the Flight Plan 5) V4 will now be made the active leg of the flight plan. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to highlight SLN. The TO ...
Page 102 - Figure 7-22 Turn on to Active Leg
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-10 6) The aircraft continues on heading 290º. When 2.0 nm from the intercept, the XTK will disappear from the HSI and the CDI will be positioned on the last dot indicating a 2.0 nm distance from the ce...
Page 103 - Figure 7-25 HYS to LAA Leg Active; Figure 7-26 Direct To OPSHN; Figure 7-27 Enter VNV Altitude
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-11 10) At Lamar VOR (LAA) V263 will be intercepted. See Figure 7-25. Figure 7-25 HYS to LAA Leg Active 11) ATC grants clearance to proceed direct to OPSHN intersection to begin the arrival procedure an...
Page 104 - Figure 7-28 Enter VNV Offset Distance; PROC
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-12 f) Press the ENT Key. The cursor is now displayed in the VNV offset field as shown in Figure 7-28. Figure 7-28 Enter VNV Offset Distance g) Enter the offset, or distance from the waypoint at which th...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-13 b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 7-30. Figure 7-30 Procedures Window c) Press the ENT Key. A list of available approaches for the destination airport will be displayed a...
Page 106 - Figure 7-33 Loaded Approach; Figure 7-34 Vertical Guidance is Active to the FAF
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-14 h) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen in Figure 7-33. Figure 7-33 Loaded Approach 13) Note the altitude constraints associate...
Page 107 - VNV PROF; Figure 7-35 Adjusting the Descent
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-15 a) Press the VNV PROF Softkey to place the cur- sor in the target vertical speed field (VS TGT) as shown in Figure 7-35. b) At this point, the descent vertical speed can be selected, or the FPA can b...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-16 16) Upon reaching TOD, a descent vertical speed is established which places the VSI pointer in line with the RVSI as shown in Figure 7-38. Figure 7-38 VDI & RVSI Showing Correctly Established De...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-17 19) After passing OPSHN, the next leg of the arrival will turn magenta as shown in Figure 7-41. The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure...
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)
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-18 21) Upon passing PYNON the approach procedure will automatically become active. The approach may be activated at any point to proceed directly to the IAF. In this example, the aircraft has progresse...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-19 23) After crossing FALUR the next waypoint is the FAF. The flight phase changes to LPV on the HSI indicating the current phase of flight is in Approach Mode and the approach type is LPV. CDI scaling c...
Page 112 - SUSP; Figure 7-48 Missed Approach Active
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-20 In this missed approach procedure, the fix immediately following the MAP (in this case ‘6368 FT ’) is not part of the published procedure. It is simply a fix that defines a leg which guides the aircra...
Page 113 - Figure 7-49 Establishing the Holding Pattern; AIRPORT INFORMATION; Figure 7-53 Airport Information Page; Select the Airport Information Page
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-21 26) The aircraft continues climbing to “AT or ABOVE” 10,000 feet at MOGAL. A holding pattern will be established at the MAHP (MOGAL) as shown in Figure 7-49. Figure 7-49 Establishing the Holding Pat...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-22 Select an Airport from the Active Flight Plan 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the small FMS Knob to the left to display a list of fl...
Page 115 - Access Runway Information; INTERSECTION INFORMATION; Select the Intersection Information Page; Figure 7-57 Intersection Information Page; Access Information on an Intersection
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-23 Access Runway Information 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to place the cursor on the ‘RUNWAYS’ identifier field. 3...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-24 7.6 NDB INFORMATION Figure 7-58 NDB Information Page Select the NDB Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the third rectang...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-25 7.8 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user defined waypoints. 7.9 NEAREST AIRPORTS Figure 7-60 Nearest Airports Page Nearest Ai...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-26 Nearest Airports Information on the PFD Primary COM Frequency Identifier Airport Symbol Bearing TO Distance Runway Length Figure 7-61 Nearest Airports Window Press the NRST Softkey to display the PFD...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-27 7.11 NEAREST NDB Figure 7-63 Nearest NDB Page Select the Nearest NDB Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the third rectangular page ...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-28 3) Press the FMS Knob to remove the flashing cursor. 7.13 NEAREST USER WAYPOINT Figure 7-65 Nearest User Waypoints Page Select the Nearest User Waypoint Page 1) Turn the large FMS Knob to select the...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 7 – NAVIGATION 7-29 7.15 NEAREST AIRSPACES Figure 7-67 Nearest Airspaces Page Select the Nearest Airspaces Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the seven...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 8-1 SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING The following discussions pertain to the Multi Function Display, unless otherwise indicated. 8.1 USER DEFINED WAYPOINTS Figure 8-1 User WPT Information Page Select the...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 8-2 SECTION 8 – FLIGHT PLANNING Create User Waypoints from the Navigation Map Page 1) With the Navigation Map Page displayed, push the Joystick to activate the panning function. The target pointer is displayed at the present a...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 8-3 SECTION 8 – FLIGHT PLANNING turn the large FMS Knob to highlight ‘CANCEL’ and press the ENT Key. 8.4 ACTIVATE A FLIGHT PLAN LEG 1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor and turn the la...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 8-4 SECTION 8 – FLIGHT PLANNING 8.7 CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the MFD 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the NEW Softkey to display ...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 8-5 SECTION 8 – FLIGHT PLANNING 8.8 ENTER AN AIRWAY IN A FLIGHT PLAN 1) Press the FPL Key to display the active flight plan or display a stored flight plan. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Kno...
Page 128 - LD AIRWY; Figure 8-17 Select Desired Airway; Figure 8-19 Airway Added to Flight Plan; LOAD A DEPARTURE
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 8-6 SECTION 8 – FLIGHT PLANNING 7) Press the LD AIRWY Softkey. A list of available airways is now displayed. Figure 8-17 Select Desired Airway 8) Turn either FMS Knob to highlight the desired airway. 9) Press the ENT Key. A li...
Page 129 - Figure 8-20 Store Flight Plan Confirmation; Figure 8-21 Remove Waypoint Confirmation
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 8-7 SECTION 8 – FLIGHT PLANNING 8.13 STORE A FLIGHT PLAN 1) After creating a flight plan on either the PFD or MFD, it may be saved by pressing the MENU Key. 2) Turn the large FMS Knob to highlight ‘Store Flight Plan’ and press ...
Page 130 - COPY A FLIGHT PLAN; DELETE A FLIGHT PLAN; GRAPHICAL FLIGHT PLAN CREATION; ABOVE; Figure 8-22 Trip Planning Page; Starting WPT
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 8-8 SECTION 8 – FLIGHT PLANNING 8.17 COPY A FLIGHT PLAN 1) From the Flight Plan Catalog press the FMS Knob to activate the cursor 2) Turn the large FMS Knob to highlight the flight plan to be copied. 3) Press the COPY Softkey. ...
Page 131 - The Page Mode must be set to MANUAL
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 8-9 SECTION 8 – FLIGHT PLANNING 4) For Direct-to planning, press the WPTS Softkey and verify that the starting waypoint field indicates ‘P.POS’ (present position). If necessary, press the MENU Key and select ‘Set WPT to Present...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 9-1 SECTION 9 – PROCEDURES SECTION 9: PROCEDURES 9.1 ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT DEPARTURE’. 3) Press the ENT Key. 4) I...
Page 134 - Knob to; to select the desired; Not all approaches in the database are approved for GPS; WAAS systems only
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 9-2 SECTION 9 – PROCEDURES Figure 9-3 Select Arrival 7) A second window is displayed listing available transitions for the arrival. Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key. Figur...
Page 135 - Figure 9-6 Selecting an Approach Procedure; Figure 9-7 Selecting an Approach Transition; Activate An Approach in the Active Flight Plan
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 9-3 SECTION 9 – PROCEDURES Load and/or Activate an Approach Procedure 1) Press the PROC Key. 2) Turn the large FMS Knob to highlight ‘SELECT APPROACH’. 3) Press the ENT Key. 4) If a flight plan is active, the destination airpor...
Page 137 - SECTION 10: HAZARD AVOIDANCE; CUSTOMIZING THE HAZARD; Menu; Figure 10-1 Page Menu; Strike is less than 6 seconds old
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-1 SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1) With the Navigation Map Page displayed, press the MENU Key to display the Navigation Map Page Menu ....
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-2 SECTION 10 – HAZARD AVOIDANCE At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The presence of Stormscope lightning data is indicated by the annunciation ‘LTNG < ...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-3 SECTION 10 – HAZARD AVOIDANCE 10.3 XM WEATHER (OPTIONAL) WARNING: XM Weather is not intended to be used for hazardous weather penetration. Weather information provided by XM Radio Service is approved only for weather avoi...
Page 140 - Figure 10-9 Weather Data Link Page; NEXRAD Limitations; Strikes depicted represent cloud to ground
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-4 SECTION 10 – HAZARD AVOIDANCE Displaying Weather on the Weather Data Link Page Select the Weather Data Link Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the fourth re...
Page 141 - Joystick; Weather Products and Symbols
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-5 SECTION 10 – HAZARD AVOIDANCE CELL MOV – Pressing the CELL MOV Softkey shows storm cell movement by displaying an arrow pointing in the direction of predicted movement. The display is updated every 12 minutes. SIG/AIR – P...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-6 SECTION 10 – HAZARD AVOIDANCE • Freezing Levels• Winds Aloft• County Warnings• Cyclone Warnings Figure 10-10 Weather Product Symbols Echo Top (Cloud Top and Echo Top Mutually Exclusive) The XM Information Page in the AUX ...
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.
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-7 SECTION 10 – HAZARD AVOIDANCE 10.4 TRAFFIC INFORMATION SERVICE (TIS) NOTE: Traffic Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site. Displaying...
Page 144 - Refer to the Avidyne; Figure 10-12 Traffic Map Page
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-8 SECTION 10 – HAZARD AVOIDANCE 10.5 AVIDYNE ® TAS600 SERIES Refer to the Avidyne ® TAS600 Series Pilot’s Guide for a detailed discussion of the TAS system and an explanation of the aural alerts. Displaying Traffic on the Tr...
Page 145 - TERRAIN AND OBSTACLE PROXIMITY; Terrain data is not displayed when the; Figure 10-13 Obstacle Symbols; Color
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-9 SECTION 10 – HAZARD AVOIDANCE 10.6 TERRAIN AND OBSTACLE PROXIMITY NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. Displaying Terrain and Obstacles on th...
Page 146 - Displaying Terrain on the TAWS Page
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-10 SECTION 10 – HAZARD AVOIDANCE 10.7 TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY (OPTIONAL) NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. NOT...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-11 SECTION 10 – HAZARD AVOIDANCE Color Terrain/Obstacle Location Red Terrain/Obstacle above or within 100’ below or above aircraft altitude. Yellow Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. Bl...
Page 148 - TAWS System; OK; Reduced Required Terrain Clearance (RTC) and; Enroute
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-12 SECTION 10 – HAZARD AVOIDANCE TAWS Inhibit Flying VFR into an area where unique terrain exists could cause the system to annunciate a nuisance alert. When TAWS is inhibited, only FLTA and PDA alerts are disabled. Inhibit...
Page 149 - Figure 10-18 PDA Alerting; Negative Climb Rate After Takeoff; Don’t Sink
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-13 SECTION 10 – HAZARD AVOIDANCE Premature Descent Alert (PDA) A Premature Descent Alert is issued when the system detects that the aircraft is significantly below the normal approach path to a runway. The PDA alert mode fun...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-14 SECTION 10 – HAZARD AVOIDANCE ���� ��� ��� ��� ��� ��������������������������� �������������������� �� � ��� � ��� � ��� � ��� � ���� � ���� � ��� ������������ ������������ Figure 10-20 Negative Climb Rate ���� ��� ��� �...
Page 151 - Alert Type
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-15 SECTION 10 – HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages. Alert Type PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Au...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 10-16 SECTION 10 – HAZARD AVOIDANCE The following system status annunciations may also be issued. Alert Type PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS A...
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
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 11 – ABNORMAL OPERATION 11-1 SECTION 11: ABNORMAL OPERATION 11.1 REVERSIONARY MODE Should a system detected failure occur in either display, the G1000 automatically enters reversionary mode. In reversionary mode, criti...
Page 154 - Figure 11-2 Extreme Pitch Indication
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 11 – ABNORMAL OPERATION 11-2 11.2 ABNORMAL COM OPERATION When a COM tuning failure is detected by the system, the emergency frequency (121.500 MHz) is automatically loaded into the active frequency field of the COM radi...
Page 155 - Dead Reckoning Mode will only function in; Symbolic Aircraft
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A SECTION 11 – ABNORMAL OPERATION 11-3 11.6 DEAD RECKONING While in Enroute or Oceanic phase of flight, if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position, the system will automatically revert t...
Page 157 - SECTION 12 – ANNUNCIATIONS
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 12-1 SECTION 12 – ANNUNCIATIONS & ALERTS SECTION 12: ANNUNCIATIONS & ALERTS NOTE: The Airplane Flight Manual Supplement s u p e r s e d e s i n f o r m a t i o n f o u n d i n t h i s document. Figure 12-1 G1000 Alerti...
Page 158 - ALERT LEVEL DEFINITIONS
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 12-2 SECTION 12 – ANNUNCIATIONS & ALERTS • Audio Alerting System: The G1000 system issues audio alert tones when specific system conditions are met. See the Alert Levels Definitions section for more information. 12.1 ALERT L...
Page 159 - AIRCRAFT ALERTS; The following alerts are configured specifically for; WARNING Alerts; L FUEL LOW; Message Advisory Alerts; PFD FAN FAIL
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 12-3 SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 AIRCRAFT ALERTS The following alerts are configured specifically for the Diamond DA40 aircraft. See the Flight Manual Supplement for information regarding pilot responses. WARNIN...
Page 160 - The following alert annunciations appear in the AFCS; Condition; If; Figure 12-5 AFCS System Status Annunciation; System Status Annunciation
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 12-4 SECTION 12 – ANNUNCIATIONS & ALERTS 12.4 AFCS ALERTS System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD. Condition Annunciation Description Pitch Fail...
Page 162 - When an LRU or an LRU function fails, a large red
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 12-6 SECTION 12 – ANNUNCIATIONS & ALERTS TAWS System Status Annunciations Alert Type PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled ...
Page 163 - System Annunciation
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 12-7 SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment This annunciation will only be seen when the autopilot is engaged. The annunciation indicates an AHRS monitor has detected an abnormal flight parameter, p...
Page 164 - Figure 12-6 G1000 System Failure Annunciations; Aural Alert; “Vertical track”
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 12-8 SECTION 12 – ANNUNCIATIONS & ALERTS A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-6 illustrates all possible flags and the responsible LRUs. Figure 12-6 G1000 System Failure Annunciati...
Page 168 - Message
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 12-12 SECTION 12 – ANNUNCIATIONS & ALERTS GMA 1347 Message Advisories Message Comments GMA1 FAIL – GMA1 is inoperative. The audio panel self-test has detected a failure. The audio panel is unavailable. The G1000 system sho...
Page 172 - TRUE APR
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A 12-16 SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63W Message Advisories (Cont.) Message Comments COM1 TEMP – COM1 over temp. Reducing transmitter power. The system has detected an over temperature condition in COM1 and/or COM...
Page 179 - INDEX; Signal augmentation 5-2
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A Index-1 INDEX A Abnormal COM operation 11-2Activate a flight plan 8-3Active flight plan 8-2ADF 1-6, 1-7, 4-3ADVISORY 12-1Advisory alerts 12-3AFCS 1-3, 6-1, 6-2, 6-23, 12-4Age 10-6AHRS 12-18, 12-19Aircraft alerts 12-3AIRMET 10-5A...
Page 180 - Load the nearest ARTCC frequency
Garmin G1000 Cockpit Reference Guide for the DA40/40F 190-00324-07 Rev. A Index-2 INDEX G GA 6-1Glidepath 2-6, 7-19Glidepath Mode 6-14, 6-20Glidepath Mode (GP) 6-31Glideslope 2-6, 7-19Glideslope Mode 6-15, 6-20, 6-30Glidesope Indicator 2-2GMA 1347 1-1Go Around 6-1Go Around Mode 6-32–6-33Go Around Mo...
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