Garmin Software Version 0370.17- Manuals

Page 3 - Garmin G1000 Cockpit Reference Guide for the DA42

Garmin G1000 Cockpit Reference Guide for the DA42 Copyright © 2004-2007 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reﬂects the operation of System Software version 0370.17 or later for the DA42. Some differences in operation may be observed when comparing the information in th...

Page 7 - RECORD OF REVISIONS; Part Number

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B RR-1 RECORD OF REVISIONS Part Number Change Summary 190-00406-01 Rev A Rev B Added DME capabilityAdded BRG1/BRG2 pointersChanged Airspeed Trend VectorChanged Altitude Trend VectorAdded Checklist capabilityAdded Flight ID capabilit...

Page 8 - Revision Date of Revision Affected Pages

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B RR-2 RECORD OF REVISIONS Revision Date of Revision Affected Pages Description B April, 2007 Added pages 10- 12 through 10-26 Page 12-4 Added GWX 68 Color Weather Radar Added Check Gear message

Page 9 - TABLE OF CONTENTS; Section 1: System Overview

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B i TABLE OF CONTENTS Section 1: System Overview ......................................... 1-1 1.1 PFD/MFD Controls ................................................... 1-2 1.2 PFD Softkeys ..............................................

Page 10 - ii; Section 7: Navigation

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B ii TABLE OF CONTENTS 6.6 Example Procedures Using AFCS ....................... 6-13 Departure ................................................................. 6-14Intercepting a VOR Radial ...........................................

Page 11 - iii; Honeywell; Section 11: Abnormal Operation

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B iii TABLE OF CONTENTS 10.3 XM Weather (Optional) ............................................ 10-3 Displaying METAR and TAF Information on the Airport Information Page ........................................... 10-3Displaying Wea...

Page 12 - Blank Page

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B iv TABLE OF CONTENTS Blank Page

Page 13 - SECTION 1; 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 DA42 190-00406-05 Rev. B 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 more ea...

Page 14 - MFD Only

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 1-2 SECTION 1 SYSTEM OVERVIEW 1.1 PFD/MFD CONTROLS MFD Only (with optional GFC 700) Figure 1-1 PFD/MFD Controls 4 2 1 6 5 7 9 8 3 17 12 13 11 10 16 15 14 20 21 19 18 26 25 24 22 23 28 27

Page 16 - Softkey OFF

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 1-4 SECTION 1 SYSTEM OVERVIEW (16) ENT Key – Accepts a menu selection or data entry. This key is used to approve an operation or complete data entry. It is also used to conﬁrm selections and information entries. (17) Dual ALT Knob...

Page 17 - Figure 1-3 PFD Softkey Flow Chart – 1; PFD

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 1-5 SECTION 1 SYSTEM OVERVIEW INSET OFF TOPO TRAFFIC TERRAIN DCLTR DCLTR-2 DCLTR-3 DCLTR-1 NEXRAD Press the BACK or OFF Softkey to return to the top level softkeys XM LTNG STRMSCP BACK ALERTS (optional) (optional) (optional) Figur...

Page 18 - Figure 1-4 PFD Softkey Flow Chart – 2; OBS; Figure 1-5 PFD Softkey Flow Chart – 3; XPDR

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 1-6 SECTION 1 SYSTEM OVERVIEW PFD Press the STD BARO or BACK softkeys to return to the top level softkeys Press the DFLTS Softkey to change the PFD metric values to standard ARC HSI 360 HSI STD BARO BACK ALERTS BRG2 BRG1 METRIC DF...

Page 20 - Figure 1-6 MFD Softkeys

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 1-8 SECTION 1 SYSTEM OVERVIEW Figure 1-6 MFD Softkeys MAP DCLTR TRAFFIC TOPO TERRAIN DCLTR-2 DCLTR-3 DCLTR-1 BACK Press to return to the top softkey level CHKLIST EXIT EMERGCY ENGINE DCLTR MAP ENGINE CHKLIST CLR DONE The DONE Soft...

Page 21 - Figure 1-7 Page Group Icon

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 1-9 SECTION 1 SYSTEM OVERVIEW 1.4 MFD PAGE GROUPS 1) Turn the large FMS Knob until the desired page group is selected. 2) Turn the small FMS Knob to select pages within the group. See Figure 1-7. Figure 1-7 Page Group Icon Map Pag...

Page 22 - DATABASE UPDATES; Aviation Database Update; Figure 1-9 Database Update Prompt; ENT; Figure 1-10 Database Update Confirmation; Terrain and Obstacle Database Updates; These databases are not stored internally in the MFD; TOPO

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 1-10 SECTION 1 SYSTEM OVERVIEW 1.6 DATABASE UPDATES Aviation Database Update NOTE: The display downloads the aviation database and stores it internally. The aviation database SD card is not required to remain in the display after ...

Page 23 - Figure 1-11 Power-Up Splash Screen Window

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 1-11 SECTION 1 SYSTEM OVERVIEW 3) Acknowledge the Power-up Page agreement by pressing the ENT Key or the right most softkey. 4) At the MAP – NAVIGATION MAP page, select the MAP Softkey and check to make sure that the TOPO and TERR...

Page 25 - SECTION 2; SECTION 2: FLIGHT INSTRUMENTS; Figure 2-1 Default PFD Information

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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 14 15...

Page 26 - Figure 2-2 Additional PFD Information; Next Waypoint

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 2-2 SECTION 2 FLIGHT INSTRUMENTS Figure 2-2 Additional PFD Information 4 7 8 1 3 6 2 12 Trafﬁc Annunciation 2 4 3 1 8 Inset Map Selected Course Box Annunciation Window 7 Alerts Window Vertical Deviation/Glideslope IndicatorMarker ...

Page 27 - 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 DA42 190-00406-05 Rev. B 2-3 SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Figure 2-4 Airspeed Indicator Actual Airspeed Airspeed Trend Vector True Airspeed Box Vspeed References Speed Ranges Vyse (Blue Line) Vmc (Red Line) Selected Airspeed Bug Sel...

Page 28 - Figure 2-7 Altimeter; Altitude Reference Bug; Set the Altitude Reference Bug; Altitude Trend Vector; BARO; Altitude Alerting; Figure 2-8 Altitude Alerting Visual Annunciations; Barometric Minimum Descent Altitude

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 2-4 SECTION 2 FLIGHT INSTRUMENTS 2.3 ALTIMETER Altitude Reference Box Altitude Trend Vector Current Altitude Barometric Setting Box Figure 2-7 Altimeter Altitude Reference Bug Altitude Reference Bug The Altitude Reference Bug can ...

Page 29 - Figure 2-9 Barometric Minimum Descent Altitude; INDICATOR; Figure 2-10 Marker Beacon and Vertical Deviation; VERTICAL SPEED INDICATOR; Figure 2-11 Vertical Speed Indicator; VS

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 2-5 SECTION 2 FLIGHT INSTRUMENTS Within 100 ft Altitude Reached Within 2500 ft Figure 2-9 Barometric Minimum Descent Altitude Alerting Visual Annunciations Barometric Minimum Box Barometric Minimum Bug 2.4 VERTICAL DEVIATION/GLIDE...

Page 30 - HORIZONTAL SITUATION INDICATOR; Figure 2-12 Horizontal Situation Indicator

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 2-6 SECTION 2 FLIGHT INSTRUMENTS 2.7 HORIZONTAL SITUATION INDICATOR (HSI) The HSI compass can be displayed as a 360° rose or 140° arc by pressing the PFD Softkey, followed by the 360 HSI or the ARC HSI Softkey. Figure 2-12 Horizon...

Page 31 - Figure 2-14 Standard-Rate Turn Indication; Course Pointer; Figure 2-15 Arc CDI and Compass Rose CDI; Bearing Pointers and Information Windows; Figure 2-16 HSI with Bearing Information

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 2-7 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 tur...

Page 32 - Figure 2-17 BRG1 Information Window; To display the DME Information Window, press the; Figure 2-19 DME Information Window; Navigation Source; • INTEG – GPS information is either not present or; The; Softkey is only displayed when

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 2-8 SECTION 2 FLIGHT INSTRUMENTS Distance to Bearing Source Waypoint Identiﬁer Bearing Source Pointer Icon Figure 2-17 BRG1 Information Window Distance to Bearing Source Waypoint Identiﬁer Pointer Icon Bearing Source Figure 2-18 B...

Page 33 - SECTION 3 – ENGINE; SECTION 3: ENGINE INDICATION; ENGINE; Figure 3-1 ENGINE Display; ENGINE SYSTEM DISPLAY; Figure 3-2 SYSTEM Display

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-1 SECTION 3: ENGINE INDICATION SYSTEM (EIS) 3.1 ENGINE DISPLAY In all cases green indicates normal operation, yellow indicates caution, and red indicates warning. Pressing the ENGINE So...

Page 34 - If optional auxiliary fuel tanks are; If desired, use the; Fuel calculations do not use the aircraft

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3-2 3.3 FUEL DISPLAY NOTE: If optional auxiliary fuel tanks are installed, the fuel remaining can be adjusted up to a maximum of 76.4 gal; the Fuel Quantity Indicator does not account for...

Page 35 - TRANSPONDER; The NAV/COM controls and frequency boxes are

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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 COM...

Page 36 - Figure 4-2 Frequency Fields

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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 Selec...

Page 37 - RADIO STATUS INDICATIONS; Figure 4-5 Radio Status Indications; AUTOMATIC SQUELCH; COM; OPTIONAL NAV RADIOS; DME

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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 whit...

Page 38 - Figure 4-8 Radio Tuning Window; Auto-tuning on the PFD; FMS

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 4-4 SECTION 4 – NAV/COM & TRANSPONDER DME Radio (optional) The tuning window is displayed by pressing the ADF/ DME Softkey (if no ADF is installed, the softkey will be labeled DME ). Figure 4-8 Radio Tuning Window Change the D...

Page 39 - Figure 4-11 Ground Mode; Code Number and; Figure 4-12 Standby Mode; Manual ON Mode; ON Mode; 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

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 4-5 SECTION 4 – NAV/COM & TRANSPONDER 4.7 TRANSPONDER Mode Selection The STBY , ON , ALT, VFR, CODE, and IDENT softkeys can be accessed by pressing the XPDR Softkey. Ground Mode (Automatic) GND is displayed when the aircraft i...

Page 40 - Manual Code Entry; Following is a list of important codes:; Flight ID Reporting; If so configured, the Flight ID may be entered in the; Flight ID

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 4-6 SECTION 4 – NAV/COM & TRANSPONDER Manual Code Entry 1) P r e s s t h e XPDR S o f t ke y t o d i s p l a y t h e transponder Mode Selection softkeys. 2) P r e s s t h e CODE S o f t ke y t o d i s p l a y t h e transponder...

Page 41 - SECTION 5 – AUDIO PANEL; SECTION 5: AUDIO PANEL; Figure 5-1 Audio Panel Controls

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 5-1 SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transmitters (COM3 MIC is unavailable) Transceiver Audio (COM 3 is unavailable) Split COM (Not recommended on the DA42) Telephone (Unavailable) Marker Beacon/Mute Passenger Addres...

Page 42 - COM RADIO SELECTION; Figure 5-2 Transceivers; SPLIT COM FUNCTION; NOTE; Split COM performance is affected by; Figure 5-3 Split COM Function; MARKER BEACON RECEIVER; Figure 5-4 Marker Beacon Annunciators on the PFD

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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 Key...

Page 43 - HI SENS; Figure 5-5 Marker Beacon; NAV RADIO AUDIO SELECTION; Table 5-1 ICS Isolation Modes; PILOT; Figure 5-7 ICS Isolation

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 5-3 SECTION 5 – AUDIO PANEL Marker Beacon Signal Sensitivity The HI SENS Key can be pressed for increased marker beacon signal sensitivity. Figure 5-5 Marker Beacon 5.4 NAV RADIO AUDIO SELECTION Pressing DME , ADF , NAV1 , or NAV2...

Page 44 - INTERCOM SQUELCH CONTROL

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 5-4 SECTION 5 – AUDIO PANEL 5.6 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ Key to light the annunciator. Pressing the small VOL/SQ Knob now switches between volume and squelch adjustme...

Page 45 - SECTION 6 – AUTOMATIC; SECTION 6: AUTOMATIC FLIGHT; Figure 6-1 AFCS Keys; MODE ANNUNCIATIONS

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-1 SECTION 6: AUTOMATIC FLIGHT CONTROL In addition to the AFCS (Automatic Flight Control System) keys on the MFD, as discussed in the System Overview section, the following buttons and switche...

Page 46 - Figure 6-3 PFD AFCS Display; AP; Figure 6-4 Autopilot Engaged Annunciation; Automatic Disengagement; AP DISC; Figure 6-5 Automatic Disconnect Annunciation

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-2 Figure 6-3 PFD AFCS Display Armed Mode Active Mode Autopilot Status Mode Reference Active Mode Armed Mode System Status Field (see Annunciations & Alerts) Flight Director Command Bars A...

Page 47 - Figure 6-6 Manual Disconnect Annunciation; Manual Disconnect; Figure 6-7 CWS Annunciation; Control Wheel Steering; Yaw Damper; Yaw Damper is active.; Figure 6-8 Yaw Damper Active; Yaw Damper is disengaging.; Figure 6-9 Yaw Damper Disengagement; PITCH AXIS MODES; AFCS Key

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-3 Manual Disengagement The autopilot may also be manually disengaged by pressing the AP DISC Button, the GA Button, the AP TRIM ARM Switch, or by pressing the AP Key on the MFD. Manual diseng...

Page 48 - Flight Director; Figure 6-11 Pitch Hold Mode; CWS

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-4 pitch axis mode when the autopilot and/or ﬂight director is engaged. Pitch Hold Mode (PIT) 1) Press the AP or FD Key. ‘PIT’ will be displayed in green in the Active Mode ﬁeld of the AFCS St...

Page 49 - ALT; Figure 6-12 Altitude Hold Mode; If the Selected Altitude is captured during; Button after the Selected Altitude is

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-5 Altitude Hold Mode (ALT) 1) Press the ALT Key. The ﬂight director is activated (if not already active) and ‘ALT’ is now displayed in green in the Active Mode ﬁeld with the current altitude ...

Page 50 - Figure 6-13 Vertical Speed Hold Mode

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-6 Vertical Speed Mode (VS) 1) Press the VS Key. The ﬂight director is now activated (if not already active) and ‘VS’ is displayed in green in the Active Mode ﬁeld and the Vertical Speed Bug w...

Page 51 - toward; FLC; Figure 6-14 Flight Level Change Mode; Altitude Hold Mode is armed.

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-7 Flight Level Change Mode (FLC) 1) Select the desired altitude by turning the ALT Knob to set the altitude in the Altitude Select box. This altitude must be selected ﬁrst because Flight Leve...

Page 52 - GA; Pressing the CWS Button while Glideslope; APR

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-8 Go-around Mode (GA) Pressing the GA Button (located on the thottle handle) engages the ﬂight director in a wings level, pitch up attitude. Go-Around Mode disengages the autopilot, and arms ...

Page 53 - Mode annunciations for active roll axis modes are; Figure 6-16 Roll Hold Mode

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-9 6.5 ROLL AXIS MODES Mode annunciations for active roll axis modes are shown in green during normal operation. AFCS Key AFCS Mode Annunciation FD/AP only Roll Hold (Default) ROL HDG Heading ...

Page 54 - Figure 6-17 Heading Select Mode; HDG

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-10 Heading Select Mode (HDG) 1) Turn the HDG Knob to move the heading bug on the HSI to the desired heading. When the knob is turned, the Selected Heading Box will appear and remain for three...

Page 55 - NAV; When making a backcourse approach, set; Navigation Mode Armed

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-11 Navigation Mode (GPS, VOR, LOC, or BC) Pressing the NAV Key activates the Navigation Mode. Navigation Mode acquires and tracks the selected navigation receiver on the HSI (GPS, VOR or LOC)...

Page 56 - Approach Mode acquires and tracks the selected; While using Approach Mode, the; See the Example Procedures Using AFCS section for

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-12 Approach Mode (GPS, VAPP or LOC) Approach Mode acquires and tracks the selected navigation receiver on the HSI (GPS, VOR, or LOC). This mode uses the selected navigation receiver deviation...

Page 57 - EXAMPLE PROCEDURES USING AFCS; This section provides a scenario-based set of procedures; Figure 6-20 Flight Plan Overview

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-13 6.6 EXAMPLE PROCEDURES USING AFCS This section provides a scenario-based set of procedures showing various autopilot modes used during a ﬂight. In this scenario, the aircraft departs Reid-...

Page 58 - Figure 6-21 Departure

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-14 Departure Climb to the Selected Altitude and Fly an Assigned Heading 1) Upon takeoff, set the Selected Altitude to 7000 feet using the ALT Knob. To have the autopilot capture this altitude...

Page 59 - Changing the HSI mode cancels; CDI; Figure 6-22 Intercepting a VOR

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-15 Intercepting a VOR Radial NOTE: Changing the HSI mode cancels Navigation Mode and causes the flight director to revert to Roll Hold Mode. During climb-out, the autopilot continues to ﬂy th...

Page 60 - Figure 6-23 Transition to GPS Flight Plan

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-16 Flying a GPS Flight Plan 1) Enter Panoche VORTAC (PXN) and Clovis VORTAC (CZQ) into the GPS ﬂight plan, in preparation to intercept this leg. 2) Transition from VOR to GPS Navigation Mode....

Page 61 - While flying the GPS leg from Panoche VORTAC to; Knob, set the Selected Altitude; Key to activate Flight Level; Figure 6-24 FLC Descent; ) Reduce power to allow descent in Flight Level

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-17 Flight Level Change (Descent) While ﬂying the GPS leg from Panoche VORTAC to Clovis VORTAC, the aircraft is cleared to make a descent to 3000 feet in preparation for the approach to KFAT. ...

Page 62 - Figure 6-25 ILS Approach to KFAT

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-18 ILS Approach 1) Transition from GPS Navigation Mode to Heading Select Mode.a) Load the Runway 29R ILS approach for KFAT into the Flight Plan. b) Select ‘Vectors to Final’ for the transitio...

Page 64 - AFCS ANNUNCIATIONS AND ALERTS; AFCS Status Alerts; The following annunciations (listed in order of; Figure 6-27 AFCS Status Annunciation; AFCS Status

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-20 6.7 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 indicators. ...

Page 65 - Overspeed protection is provided in situations where; Figure 6-28 Overspeed Annunciation; Airspeed

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 6 – AUTOMATIC FLIGHT CONTROL 6-21 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 without ...

Page 67 - SECTION 7 – NAVIGATION; 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

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 7 – NAVIGATION 7-1 SECTION 7: NAVIGATION The following discussions pertain to the Multi Function Display, unless otherwise indicated. 7.1 NAVIGATION MAP PAGE Select the MAP Page Group 1) Turn the large FMS Knob until ‘ MAP...

Page 68 - Figure 7-3 Canceling Direct-to Navigation; Direct-to Navigation from the PFD

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 7 – NAVIGATION 7-2 3) Turn the small FMS Knob to display a list of waypoints or airports. 4) Continue turning the small FMS Knob to scroll through the list and highlight the desired waypoint or airport. 5) Press the ENT Ke...

Page 69 - AIRPORT INFORMATION; Figure 7-5 Airport Information Page; Select the Airport Information Page

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 7 – NAVIGATION 7-3 7.3 AIRPORT INFORMATION Figure 7-5 Airport Information Page Select the Airport Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the ﬁrst re...

Page 70 - INTERSECTION INFORMATION; Select the Intersection Information Page; Figure 7-6 Intersection Information Page; Select the NDB Information Page

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 7 – NAVIGATION 7-4 7.4 INTERSECTION INFORMATION Select the Intersection Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the second rectangular page icon. Fig...

Page 71 - 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

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 7 – NAVIGATION 7-5 7.6 VOR INFORMATION Figure 7-8 VOR Information Page Select the VOR Information Page 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the fourth rectangular ...

Page 72 - Figure 7-10 Nearest Airports Window

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 7 – NAVIGATION 7-6 2) Press the FMS Knob, then turn the large FMS Knob to highlight the desired airport. 3) Press the FMS Knob to remove the ﬂashing cursor. Access Runway Information for the Selected Airport 1) With the Ne...

Page 73 - NEAREST INTERSECTIONS; Figure 7-11 Nearest Intersections Page; Select the Nearest Intersections Page; Figure 7-12 Nearest NDB Page; Select the Nearest NDB Page

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 7 – NAVIGATION 7-7 7.9 NEAREST INTERSECTIONS Figure 7-11 Nearest Intersections Page Select the Nearest Intersections Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the...

Page 74 - Figure 7-13 Nearest VOR Page; NEAREST USER WAYPOINT; Figure 7-14 Nearest User Waypoints Page; Select the Nearest User Waypoint Page

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 7 – NAVIGATION 7-8 7.11 NEAREST VOR Select the Nearest VOR Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the fourth rectangular page icon. Figure 7-13 Nearest VOR Pag...

Page 75 - 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

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B SECTION 7 – NAVIGATION 7-9 3) Press the FMS Knob to remove the ﬂashing cursor. 7.13 NEAREST FREQUENCIES Figure 7-15 Nearest Frequencies Page Select the Nearest Frequencies Page 1) Turn the large FMS Knob to select the ‘NRST’ page ...

Page 77 - SECTION 8 – FLIGHT PLANNING; SECTION 8: FLIGHT PLANNING; USER DEFINED WAYPOINTS; Figure 8-1 User WPT Information Page; Select the User WPT Information Page

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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 Use...

Page 78 - 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

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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 map pointer is displayed at the present aircraft...

Page 79 - 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

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 8-3 SECTION 8 – FLIGHT PLANNING 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 large FMS Knob to highlight the desired destination waypoint. 2) Press the ...

Page 80 - 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

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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 a bl...

Page 81 - Figure 8-13 Store Flight Plan Confirmation

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 8-5 SECTION 8 – FLIGHT PLANNING 8.8 LOAD A DEPARTURE See the Procedures section for a discussion on loading and activating departure procedures. 8.9 LOAD AN ARRIVAL See the Procedures section for a discussion on loading and activa...

Page 82 - INVERT AND ACTIVATE A STORED

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 8-6 SECTION 8 – FLIGHT PLANNING 5) Once all changes have been made, press the FMS Knob to remove the cursor. 8.15 INVERT AND ACTIVATE A STORED FLIGHT PLAN 1) From the Flight Plan Catalog Page, press the FMS Knob to activate the cu...

Page 83 - Figure 8-15 Trip Planning Page; Starting WPT; The Page Mode must be set to MANUAL

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 8-7 SECTION 8 – FLIGHT PLANNING top of the page: ‘AUTOMATIC’ or ‘MANUAL’. To change the page mode, press the AUTO or MANUAL Softkey. Figure 8-15 Trip Planning Page Starting WPT Ending WPT 4) For Direct-to planning, press the WPTS ...

Page 84 - : An active flight plan or Direct-to must be; : VNAV is advisory only and cannot be; Create a Vertical Navigation Profile

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 8-8 SECTION 8 – FLIGHT PLANNING 11) The ﬂashing cursor moves to the calibrated airspeed ﬁeld. Turn the FMS Knobs to enter a calibrated airspeed. Press the ENT Key when ﬁnished. 8.20 VERTICAL NAVIGATION (VNAV) PAGE NOTE : An active...

Page 85 - 0) With the ‘TARGET ALTITUDE’ field highlighted,; Knobs to select; Key. The cursor is now placed; MAP; VNAV Page Menu Options; MENU

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 8-9 SECTION 8 – FLIGHT PLANNING in the ﬂight plan is selected. Highlight the desired waypoint. 9) Press the ENT Key. 10) With the ‘TARGET ALTITUDE’ ﬁeld highlighted, turn the small and large FMS Knobs to select the target altitude...

Page 87 - SECTION 9 – PROCEDURES; 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

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 9-1 SECTION 9 – PROCEDURES SECTION 9: PROCEDURES 9.1 ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1) With the Navigation Map Page displayed, press the FPL Key. 2) Press the LD DP Softkey. If a ﬂight plan is acti...

Page 88 - 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

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 9-2 SECTION 9 – PROCEDURES 6) 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. Figure 9-4 Select Arrival Transitio...

Page 89 - Figure 9-7 Selecting an Approach Transition; Activate an Approach in the Active Flight Plan

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 9-3 SECTION 9 – PROCEDURES 6) The cursor will move to the TRANSITIONS ﬁeld. Turn the large FMS Knob to highlight the desired transition waypoint and press the ENT Key. The “Vectors” option assumes vectors will be received to the ﬁ...

Page 91 - SECTION 10 – HAZARD; SECTION 10: HAZARD AVOIDANCE; CUSTOMIZING THE HAZARD; Figure 10-1 Page Menu

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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. The ...

Page 92 - At a map range of less than 25 nm, Stormscope; Figure 10-5 Lightning Display Range Annunciation; Stormscope Page; Figure 10-6 Stormscope Page

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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 < 25 n...

Page 93 - “Cell Mode” uses a clustering program to

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-3 SECTION 10 – HAZARD AVOIDANCE NOTE: “Cell Mode” uses a clustering program to identify clusters of electrical activity that indicate cells. Change the Viewing Mode Between 360˚ and 120˚ 1) Select the Stormscope Page.2) Press t...

Page 94 - Figure 10-8 METAR and TAF Text Displayed on the; NEXRAD

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-4 SECTION 10 – HAZARD AVOIDANCE Figure 10-8 METAR and TAF Text Displayed on the Airport (Weather) Information Page METAR Text TAF Text WX Softkey Displaying Weather on the Weather Data Link Page Select the Weather Data Link Pag...

Page 95 - Strikes depicted represent cloud to ground; to display the panning; Joystick; to place the panning arrow; Key to display pertinent information

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-5 SECTION 10 – HAZARD AVOIDANCE ECHO TOP – Press the ECHO TOP Softkey to show the location, elevation, and direction the highest radar echo. This may not indicate the top of a storm or clouds, only the highest radar return echo...

Page 96 - Note that pressing the; Key when panning; Key and; Key; Weather Products and Symbols; Figure 10-10 depicts the symbol for each weather; Figure 10-10 Weather Product Symbols; Echo Top (Cloud Top and Echo Top Mutually Exclusive); 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 DA42 190-00406-05 Rev. B 10-6 SECTION 10 – HAZARD AVOIDANCE Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that displays the text of the report. Panning over an airport with METAR information does not di...

Page 97 - Weather Product; If the G1000 is configured to use the; Displaying Traffic on the Traffic Map Page; If data is not received for a period longer than 6 seconds,; Figure 10-11 Traffic Map Page

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-7 SECTION 10 – HAZARD AVOIDANCE Weather Product Expires After (minutes) SIGMETs/AIRMETs 60 City Forecasts 60 County Warnings 60 Cyclone Warnings 60 Echo Tops 30 Freezing Levels 60 METARs 90 Lightning 30 NEXRAD 30 Radar Coverage...

Page 98 - Figure 10-12 Self Test OK Display

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-8 SECTION 10 – HAZARD AVOIDANCE Displaying Trafﬁc on the Navigation Map 1) Ensure TIS is operating. With the Navigation Map displayed, press the MAP Softkey. 2) Press the TRAFFIC Softkey. Trafﬁc will now be displayed on the map...

Page 99 - Figure 10-13 Traffic Map Page; Traffic Advisory; Avidyne; Refer to the Avidyne

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-9 SECTION 10 – HAZARD AVOIDANCE Trafﬁc, Out of Range Proximity Trafﬁc, 1000’ above & descending Trafﬁc Mode Figure 10-13 Trafﬁc Map Page “Non-Bearing” Trafﬁc (system is unable to determine bearing), distance is 8.0 nm, 1190...

Page 100 - Figure 10-15 Traffic Map Page; Displaying Traffic on the Navigation Map; TERRAIN AND OBSTACLE PROXIMITY; Terrain data is not displayed when the

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-10 SECTION 10 – HAZARD AVOIDANCE 4) Rotate the Joystick clockwise to display a larger area or rotate counter-clockwise to display a smaller area. Trafﬁc, Out of Range Proximity Trafﬁc, 1000’ above & descending Trafﬁc Mode F...

Page 101 - Color; Figure 10-18 Obstacle Symbols and Colors; Displaying Terrain and Obstacles on the; ) With the Navigation Map displayed, press the; Softkey. Terrain and obstacle

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-11 SECTION 10 – HAZARD AVOIDANCE Color Indication RED Terrain/Obstacle above or within 100’ below or above aircraft altitude. YELLOW Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. 1000' Aircraft Altitu...

Page 102 - AIRBORNE COLOR WEATHER RADAR; Weather Radar Basics; Antenna Beam Illumination; It is important to understand the concept of the; Figure 10-19 Radar Beam from 10 inch Antenna; Figure 10-19 depicts a radar beam’s characteristics.

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-12 SECTION 10 – HAZARD AVOIDANCE 10.7 AIRBORNE COLOR WEATHER RADAR (OPTIONAL) Weather Radar Basics Antenna Beam Illumination It is important to understand the concept of the antenna beam illumination. The radar beam is much lik...

Page 103 - Radar Signal Attenuation; Attenuation because of distance is due to the fact; Radar Signal Reflectivity; Precipitation; Figure 10-21 Precipitation Type and Reflectivity

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-13 SECTION 10 – HAZARD AVOIDANCE Radar Signal Attenuation Attenuation because of distance is due to the fact that the radar energy leaving the antenna is inversely proportional to the square of the distance. The reﬂected radar ...

Page 104 - Ground Returns; Figure 10-22 Angle of Incidence; A smaller incident angle gives the radar a larger

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-14 SECTION 10 – HAZARD AVOIDANCE Ground Returns The intensity of ground target returns depends upon the angle at which the radar beam strikes the ground target (Angle of Incidence) and the reﬂective properties of that target. T...

Page 105 - Safe Operating Distance; Figure 10-23 MPEL Boundary; Figure 10-24 Vertical Change in Radar Beam per Nautical Mile; Basic Antenna Tilt Setup

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-15 SECTION 10 – HAZARD AVOIDANCE Safe Operating Distance The zone in which the radiation level exceeds the US Government standard of 1 mW/cm2 is the semicircular area of at least 9.16 feet from the 10-inch antenna (Figure 10-23...

Page 106 - BLACK; Figure 10-25 Precipitation Intensity Levels; Thunderstorms; Steep Gradient; Figure 10-26 Cell Irregularities

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-16 SECTION 10 – HAZARD AVOIDANCE Weather Mapping and Interpretation Weather Display Interpretation When evaluating various target returns on the weather radar display, the colors denote precipitation intensity and rates as show...

Page 107 - Tornadoes; Operation in Weather Mode; Begin transmitting only when it; Radar Mode

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-17 SECTION 10 – HAZARD AVOIDANCE Tornadoes There are no conclusive radar target return characteristics which will identify a tornado. However, tornadoes may be present if the following characteristics are observed: • A narrow, ...

Page 108 - MODE; YES; to select the desired map range.; VERTICAL; Softkey to

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-18 SECTION 10 – HAZARD AVOIDANCE Displaying Weather on the Weather Radar Page 1) Select the Map Page Group.2) Select the Weather Radar Page.3) Select the MODE Softkey. 4) To select Weather Mapping Mode: a) While on the ground, ...

Page 109 - Vertically Scanning a Storm Cell; Vertical scanning of a storm cell should; Bearing Line; can also be used to adjust bearing from; Figure 10-31 Vertical Scan Display; Adjusting Antenna Tilt Angle; In order to make an accurate interpretation of a storm

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-19 SECTION 10 – HAZARD AVOIDANCE Vertically Scanning a Storm Cell NOTE: Vertical scanning of a storm cell should be done with the aircraft wings level to avoid constant adjustment of the Bearing Line. 1) While in the Horizontal...

Page 110 - Adjusting Antenna Tilt on the Horizontal Scan; can also be used to adjust tilt up; Adjusting Antenna Tilt on the Vertical Scan; can also be used to adjust tilt.; Figure 10-32 Adjusting Tilt on Vertical Scan Display; Scan Line

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-20 SECTION 10 – HAZARD AVOIDANCE Adjusting Antenna Tilt on the Horizontal Scan Display 1) Press the FMS Knob to activate the cursor in the TILT ﬁeld. 2) Turn the small FMS Knob to select the desired antenna tilt angle. 3) Press...

Page 111 - Adjusting Gain; Changing the gain in weather mode; Softkey to activate the cursor in; Knob to adjust the gain for the; Knob to remove the cursor.; GAIN; Softkey again to recalibrate the

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-21 SECTION 10 – HAZARD AVOIDANCE Adjusting Gain WARNING: Changing the gain in weather mode will cause precipitation intensity to be displayed as a color not representative of the true intensity. See Figures 10-33 and 10-34. Rem...

Page 112 - Sector Scan; Figure 10-35 Selecting Sector Scan Position; Antenna Stabilization

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-22 SECTION 10 – HAZARD AVOIDANCE Sector Scan 1) While in horizontal scan mode, select the BRG Softkey to display the Bearing Line and place the cursor in the BEARING ﬁeld (Figure 10-35). If the Bearing Line is not displayed, pr...

Page 113 - Weather Attenuated Color Highlight (WATCHTM); While in horizontal scan mode, this feature can be used; Figure 10-37 Horizontal Scan Without WATCHTM; Areas of Attenuated

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-23 SECTION 10 – HAZARD AVOIDANCE Weather Attenuated Color Highlight (WATCH™) While in horizontal scan mode, this feature can be used as a tool to determine areas of possible inaccuracies in displayed intensity due to weakening ...

Page 114 - Weather Alert; Figure 10-39 Weather Alert Indications; Weather Alerts; WX ALRT; Figure 10-40 Weather Alert on PFD

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-24 SECTION 10 – HAZARD AVOIDANCE Weather Alert This feature may be used to indicate the presence of heavy precipitation beyond the currently displayed range and 80 to 320 nm from the aircraft’s present position. Weather Alert t...

Page 115 - A secondary use of the weather radar system is for; Ground Map; Figure 10-41 Ground Target Return Intensity Levels; Operation in Ground Map Mode

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 10-25 SECTION 10 – HAZARD AVOIDANCE Ground Mapping and Interpretation A secondary use of the weather radar system is for the presentation of terrain. This can be a useful tool for verifying aircraft position. A “picture” of the gr...

Page 117 - SECTION 11 – ABNORMAL; 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 Airplane Flight Manual always takes

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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, critical ...

Page 118 - 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; STORMSCOPE OPERATION WITH; If heading is lost, strikes and/or cells must be cleared

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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 radio fo...

Page 119 - SECTION 12 – ANNUNCIATIONS; ALERTS

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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. The G1000 Alerting System co...

Page 120 - ALERT LEVEL DEFINITIONS

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 12-2 SECTION 12 – ANNUNCIATIONS & ALERTS 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in Diamond DA42 aircraft, uses three alert levels. • WARNING: This level of alert requires immediate pilot attention...

Page 121 - AIRCRAFT ALERTS; The following alerts are configured specifically for the; WARNING Alerts; DOOR OPEN; CAUTION Alerts; PITOT FAIL

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 12-3 SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 AIRCRAFT ALERTS The following alerts are conﬁgured speciﬁcally for the Diamond DA42 aircraft. See the Airplane Flight Manual for information regarding pilot responses. WARNING Aler...

Page 122 - DEICE LVL LO; Annunciation Advisory Alerts; PFD FAN FAIL; TIS Voice Alerts; The following voice alerts can be configured for ‘Male’

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 12-4 SECTION 12 – ANNUNCIATIONS & ALERTS Annunciation Window Text Alerts Window Message Audio Alert DEICE LVL LO De-icing ﬂuid level is low. Single Aural Tone DEIC PRES HI De-icing pressure is high. DEIC PRES LO De-icing press...

Page 123 - The following alert annunciations appear in the AFCS; Figure 12-5 AFCS System Status Annunciation; System Status Annunciation

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 12-5 SECTION 12 – ANNUNCIATIONS & ALERTS 12.3 AFCS ALERTS System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD. Alert Condition Annunciation Description Rudder M...

Page 124 - System Annunciation

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 12-6 SECTION 12 – ANNUNCIATIONS & ALERTS 12.4 G1000 SYSTEM ANNUNCIATIONS When an LRU or an LRU function fails, a large red ‘X’ is typically displayed on windows associated with the failed data. The following section describes ...

Page 126 - Figure 12-6 G1000 System Failure Annunciations

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 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. GDC 74A Air Data Computer GTX 33 Transponder OR...

Page 127 - Message

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 12-9 SECTION 12 – ANNUNCIATIONS & ALERTS MFD & PFD Message Advisories Message Comments DATA LOST – Pilot stored data was lost. Recheck settings. The pilot proﬁle data was lost. System reverts to default pilot proﬁle and se...

Page 128 - Alerts Window Message

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 12-10 SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories Alerts Window Message Comments MFD1 DB ERR – MFD1 aviation database error exists. The MFD and/or PFD detected a failure in the aviation database. Attempt to...

Page 131 - GEA 71 Message Advisories

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 12-13 SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments DGRD GPS ACC – GPS position accuracy degraded & RAIM unavailable. GPS position accuracy has been degraded and RAIM ...

Page 132 - GRS 77 Message Advisories

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B 12-14 SECTION 12 – ANNUNCIATIONS & ALERTS GTX 33 Message Advisories Alerts Window Message Comments XPDR1 CONFIG – XPDR1 conﬁg error. Conﬁg service req’d. The transponder conﬁguration settings do not match those of backup conﬁg...

Page 137 - INDEX; Signal augmentation 5-3

Garmin G1000 Cockpit Reference Guide for the DA42 190-00406-05 Rev. B Index-1 INDEX A Abnormal COM operation 11-2Activate a ﬂight plan 8-3Active ﬂight plan 8-2ADF 1-5ADVISORY 12-1Advisory alerts 12-4AFCS 1-3, 6-1, 6-2, 6-4, 6-6, 6-7, 6-9, 6-11, 6-12, 6-13, 12-5 Age 10-6AHRS 12-14Aircraft alerts 12-3...