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Garmin Software Version 0370.13 Cockpit Reference Guide

1. Turn the large FMS knob to select the next character field Repeat steps 3 and 4 until the facility name or location is selected then press the ENT key If there are duplicate names in the database a list is displayed from which to chose the desired location SECTION 7 NAVIGATION 7 To remove the flashing cursor press the FMS knob Access Runway Information 1 Press the FMS knob to activate the cursor 2 Turn the large FMS knob to place the cursor on the Runways field 3 Turn the small FMS knob to display the next runway for the selected airport 4 Continue turning the small FMS knob to select the desired runway 5 To remove the flashing cursor press the FMS knob Access Frequency Information 1 Press the FMS knob to activate the cursor 2 Turn the large FMS knob to move the cursor to the Frequencies window Turn the FMS knobs to scroll through the list placing the cursor on the desired frequency UJ 4 Press the ENT key to place the selected fre quency in the standby field of the COM or NAV window 5 To remove the flashing cursor press the FMS Knob TX transmit only RX receive only e PT part time frequency e additional information exists press the ENT key If a listed frequency has sector or altitude restrictions the frequency is preceded by an info designation Garmin G1000 Cockpit Reference Guide for the DA42 7 3 SECTION 7 NAVIGATION 1 4
2. G1000 Cockpit Reference Guide for the Diamond DA42 Copyright 2004 2005 Garmin Ltd or its subsidiaries All rights reserved This manual retlects the operation of System Software version 0370 13 or later for the DA42 Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Unit 5 The Quadrangle Abbey Park Industrial Estate Romsey Hampshire 051 9DL U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 Web Site Address www garmin com Except as expressly provided herein no part of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized com
3. INTERSECTION INFORMATION Select the Intersection Information Page IF 2 Turn the large FMS knob to select the WPT page group Turn the small FMS knob to select the second rectangular page icon 136 975 Figure 7 6 Intersection Information Page Access Information on an Intersection 1 2 3 1 4 With the Intersection Information Page dis played press the FMS knob to activate the cursor Turn the FMS knobs to enter a name for the identifier and press the ENT key Press the FMS knob to remove the flashing Cursor 1 5 NDB INFORMATION Rd ee Figure 7 7 NDB Information Page Select the NDB Information Page 1 2 Turn the large FMS knob to select the WPT page group Turn the small FMS knob to select the third rectangular page icon View Information on a Specific NDB 1 With the NDB Information Page displayed press the FMS knob to activate the cursor Turn the large FMS knob to highlight the desired selection field identifier name or clos est city Turn the FMS knobs to enter an identifier name or city and press the ENT key Press the FMS knob to remove the flashing Cursor Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 7 NAVIGATION 7 7 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on cre ating and modifying user defined waypoints 7 8 NEAREST AIRPORTS 1795 f BEGRIE NEAREST AIRPO
4. INTEG 2 7 Interrogations 4 5 K Key s 1 3 L Lightning 10 2 10 3 10 4 Load approach 8 4 Load a VOR frequency 7 8 Load departure 8 4 Load the frequency for a controlling agency 9 Load the nearest ARTCC frequency 7 9 Loss of communication code 4 5 MAP 7 1 Map panning 10 5 Marker beacon 2 4 Index 1 INDEX Messages 12 1 Message advisories 12 2 12 8 12 10 12 12 12 16 METAR 10 3 10 5 MFD 1 1 4 4 Military interceptor operations code 4 5 MKR MUTE 5 2 Mode selection softkeys 4 5 Morse code identifier 4 3 Nav Com controls 4 1 NAV1 5 2 NAV2 5 2 Navigation 7 1 Navigation status window 2 2 NAV Frequency Window 4 1 Nearest Airports Page 7 3 7 5 7 9 8 1 Nearest ARTCC amp FSS frequencies 7 8 NEXRAD 10 3 10 6 O OBS 2 7 Operation 5 2 Optional NAV radios 4 3 P Page group icon 1 8 PFD 1 1 4 1 4 4 PLAY key 5 4 PROC key 1 3 Red pointer 2 3 Remove departure arrival or approach 8 5 Replies 4 5 Reversionary mode 11 1 R indication 4 5 S Severe thunderstorm 10 5 SIGMET 10 5 Slip Skid indicator 2 3 Softkey function MFD 1 4 1 7 Speed ranges 2 3 Squelch 5 3 Store Flight Plan 8 5 Stormscope lightning data 10 2 10 3 Strike 10 2 Strike mode 10 2 System annunciations 12 1 12 5 System message advisories 12 7 T TA 10 7 TAF 10 3 Terrain 10 8 Terrain proximity 10 8 Tornado 10 5 Traffic advisory 10 7 Traffic map page 10 7 10 8 Transponder 4 5 Tr
5. Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan Press the LD WPT softkey The selected way point will be inserted at the end of the flight plan If the selected waypoint is to be placed else where in the flight plan press the FMS knob to activate the cursor Waypoints are inserted ABOVE the cursor After placing the cursor at the desired point in the list of waypoints press the LD WPT soft key TRIP PLANNING Turn the large FMS knob to select the AUX page group Turn the small FMS knob to select the first rectangular page icon 8 6 Garmin G1000 Cockpit Reference Guide for the DA42 The current page mode is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode press the AUTO or MANUAL softkey INPUT DATA myer OTHER STATS DENSITY ALT TRUE AIRSPEED WIND DIRECTION WIND SPEED HEAD WIND Figure 8 16 Trip Planning Page For Direct to planning press the WPTS softkey and verity that the from waypoint field indi cates PPOS present position If necessary press the MENU key and select Set WPT to Present Position to display P POS Press the ENT key and the flashing cursor moves to the to waypoint field Turn the FMS knobs to enter the identitier of the to waypoint and press the ENT key to accept the waypoint OR For point to point planning turn t
6. The AHRS is not receiving any or any useful GPS information Check AFMS limita information tions The G1000 system should be serviced AHRS GPS AHRS not receiving The AHRS is not receiving backup GPS information The G1000 system should be backup GPS intormation serviced AHRS GPS AHRS operating The AHRS is operating exclusively in no GPS mode The G1000 system should be exclusively in no GPS mode serviced MANIFEST GRS1 software mismatch Communication halted BACKUP PATH AHRS using backup The AHRS is using a backup communications data path The G1000 system should data path be serviced when possible AHRS SERVICE AHRS Magnetic field The AHRS earth magnetic field model is out of date Update magnetic field model model needs update when practical GEO LIMITS Too far North South no The aircraft is outside geographical limits for approved AHRS operation Heading is magnetic compass flagged as invalid GMU 44 Message Advisories Alerts Window Message Comments HDG FAULT A magnetometer fault A fault has occurred in the GMU 44 Heading is flagged as invalid The AHRS uses has occurred GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 software mismatch Communication halted The AHRS has incorrect software installed The G1000 system should be serviced The GMU 44 has incorrect sottware installed The G1000 system should be serviced 12 14 Garmin G1000 Coc
7. To display the Navigation Map Page immediately press and hold CLR MFD only 13 Dual FMS Knob Used to select the page to be viewed only on the MFD The large knob selects a page group MAP WPT AUX NRST while the small knob selects a specific page within the page group Pressing the small knob turns the selection cursor ON and OFF 14 MENU Key Displays a context sensitive list of op tions This list allows the user to access additional features or to make setting changes that relate to certain pages 15 PROC Key Selects approaches departures and ar rivals from the flight plan If a flight plan is used avail able procedures for the departure and or arrival airport are automatically suggested If a flight plan is not used the desired airport and the desired procedure may be se lected This key selects IFR departure procedures DPs arrival procedures STARs and approaches IAPs from the database and loads them into the active flight plan 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 informa tion entries 17 Dual ALT Knob Sets the reference altitude in the box located above the Altimeter The large knob selects the thousands while the small knob selects the hun dreds Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 1 SYSTEM OVERVIEW 1 2 PFD SOFTKEYS 360 HSI Softkey ON So
8. With the Nearest VOR Page selected press the FREQ softkey to highlight the VOR frequency for the selected VOR 2 Press the ENT key The selected VOR frequency is placed in the NAV standby frequency field OR Press the MENU key Select the Select Fre quency Window option and press the ENT key Press the ENT key again when the frequency field is highlighted to place the selected VOR frequency in the NAV standby field 7 12 NEAREST USER WAYPOINT 17 95 NRST 136 975 Tec pu iF S USER A S HORTH UF PAALI Figure 7 14 Nearest User Waypoints Page Select the Nearest User Waypoint Page 1 Turn the large FMS knob to select the NRST page group 2 Turn the small FMS knob to select the fifth rectangular page Icon Select a Nearest User Waypoint 1 With the Nearest User Waypoint Page selected press the FMS knob to activate the cursor Press the ENT key to select the Nearest User Waypoint The remaining information on the Nearest User Waypoint Page pertains to the selected Nearest User Waypoint NEAREST FREQUENCIES ENCIES 136 975 NEAREST ARTCC Figure 7 15 Nearest Frequencies Page Select the Nearest Frequencies Page ils Turn the large FMS knob to select the NRST page group Turn the small FMS knob to select the sixth rectangular page icon Garmin G1000 Cockpit Reference Guide for the DA42 Select and Load the Nearest ARTCC FSS or Weather Frequency 1 With the Nearest Frequen
9. misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the G1000 Flight Manual Supplement Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G1000 to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation aN WARNING The illustrations in this guide are only examples Never use the G1000 to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Airman s Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo CAUTION The GDU 1040 PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings W 2 Garmin G1000 Cockpit Reference Guide for the DA42 WARNINGS CAUTIONS amp NOTES CAUTION The Garmin G1000 does not contain any user serviceable parts Repairs should only be mad
10. 2 10 3 XM Weather Optional 10 3 Displaying METAR and TAF information on the Airport Information Page 10 3 Displaying Weather on the Weather Data Link Page 10 4 NEXRAD Limitation uen unes 10 4 Map Panning Information Weather Data Link Page 10 5 Weather Products and Symbols sseseseseereesnen 10 5 Weather Product Age 10 6 10 4 Traffic Information Service TIS 10 7 Displaying Traffic on the Traffic Map Page 10 7 Displaying Traffic on the Navigation Map 10 7 TIS Audo Alerts tn mu se ns 10 7 10 5 Terrain And Obstacle Proximity 10 8 Displaying Terrain and Obstacles on the Terrain RONDS O 10 8 Displaying Terrain and Obstacles on the Navigation IV OD RP ieee 10 8 SECTION 11 ABNORMAL OPERATION 11 1 11 1 Reversionary Mode 11 1 11 2 Abnormal COM Operation 11 2 11 3 Unusual Attitudes 11 2 Garmin G1000 Cockpit Reference Guide for the DA42 TABLE OF CONTENTS 11 4 Stormscope Operation with Loss of Heading Input 11 2 SECTION 12 ANNUNCIATIONS AND ALERTS 12 1 12 1 Alert Level Definitions 0 0 cc cee 12 2 12 2 Aircraft Alerts 12 3 WARNING AIETG na ann 12 3 CAUTION AIETE nn as tonne 12 3 Annunciation Advisory Alerts 12 4 Message Advisory Alerts 12 4 12 3 G1000 System Annunciations 12 5 Tatie VO ICIS ne sans cn 12 5 12 4 G1000 System
11. 7 6 Airport information 7 3 Airspace alerts 7 9 Airspeed indicator 2 3 Airspeed trend vector 2 3 Alerting System 12 1 Alerts 12 1 Alert levels 12 2 Altitude reference bug 2 4 Altitude trend vector 2 4 ALT knob 1 3 Annunciations 12 1 Approaches 9 2 Approach activation 4 4 Approach markers Signal augmentation 5 2 Arrivals 9 1 Attitude indicator 2 3 Audio panel 4 3 5 1 Audio panel controls ADF 5 2 DME 5 2 NAV1 5 2 NAV2 5 2 Auto tuning 4 4 Automatic squelch 4 3 Barometric setting 2 4 Base reflectivity 10 4 BKSP softkey 4 5 BRG1 2 6 BRG2 2 6 C Caution 12 1 12 2 CDI 2 7 12 16 Cell 10 2 Cell mode 10 2 Cell movement 10 5 Cloud tops 10 4 CLR key 1 3 Coast mode 10 7 Codes important 4 5 Code selection 4 5 CODE softkey 4 5 COM Frequency Window 4 1 COM knob 4 3 Controls 1 2 4 1 Create a new flight plan 8 3 8 4 Create a new user waypoint 8 1 Cyclones 10 5 D Departures 9 1 Direct to 7 1 DME 1 5 Dual CDU failure 11 2 E ECHO TOPS 10 4 Edit a flight plan 8 5 Emergency code 4 5 Engine display 3 1 ENGINE softkey 3 1 F Flight ID 4 5 Garmin G1000 Cockpit Reference Guide for the DA42 INDEX Flight Plan Catalog 9 1 9 2 FPL key 1 3 Freezing level 10 5 Frequency toggle key 1 3 4 3 Fuel remaining 3 1 G GMA 1347 1 1 Heading indication 2 6 Headset s 5 2 Hijack code 4 5 Horizontal situation indicator 2 5 HSI 2 5 Hurricanes 10 5 ICAO 4 5 ID 4 3 IDENT function 4 5
12. Aircraft altitude fang of topography eleva Ground elevation tion es y dis at present aircraft played on screen position Figure 10 13 Topography Scale Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 11 ABNORMAL OPERATION 11 1 REVERSIONARY MODE Should a system detected failure occur in either dis play the G1000 automatically enters reversionary mode In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display Minimal navigation capability is available on the reversionary mode display SECTION 11 ABNORMAL OPERATION Reversionary display mode can also be manually ac tivated by the pilot if the system fails to detect a display problem The reversionary mode is activated manually by pressing the red DISPLAY BACKUP button on the bottom of the audio panel GMA 1347 Pressing the red DISPLAY BACKUP button again deactivates reversion ary mode NOTE The Airplane Flight Manual always takes precedence over the information found in this section Normal MFD Display MFD in Reversionary Mode Figure 11 1 G1000 Reversionary Mode Failed PFD Garmin G1000 Cockpit Reference Guide for the DA42 11 1 SECTION 11 ABNORMAL OPERATION 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 r
13. FMS knobs until the desired identifier has been entered WAYPOINT INFORMATION IDENT FACILITY CITY MOST RECENT LIST tar Ez NORTH UP Figure 8 11 Waypoint Info Window 4 Press the ENT key 5 Repeat step number 3 to enter the identifier for each additional flight plan waypoint 6 When all waypoints have been entered press the FMS knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Create a new flight plan using the PFD NOTE A flight plan cannot be entered using the PFD if another flight plan is active NOTE After the first leg is entered using the PFD only it is immediately activated 1 Press the FPL key and press the small FMS knob to activate the cursor 2 Turn the small FMS knob to enter the first character of the flight plan starting identifier 3 Turn the large FMS knob to move the cursor to the next character field Turn the small FMS knob to enter the next char acter Continue this process until the desired identifier is entered 5 Press the ENT key and the cursor is now ready for entering of the next flight plan waypoint 6 Repeat steps 2 through 5 to enter the identifier for each additional flight plan waypoint 7 Once all waypoints have been entered press the FMS knob to return to the Active Flight Plan Window Figure 8 12 Creating Flight Plan on the PFD 8 8 LOAD A DEPARTURE See the Procedures section for a discussion
14. FREQ softkey and turn the FMS knobs to select the desired frequency Press the ENT key to load the frequency into the COM fre quency standby field Garmin G1000 Cockpit Reference Guide for the DA42 1 9 SECTION 7 NAVIGATION This page intentionally left blank 7 10 Garmin G1000 Cockpit Reference Guide for the DA42 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 User WPT Information Page 1 Turn the large FMS knob to select the NRST page group 2 Turn the small FMS knob to select the fifth rectangular page icon Create a New User Waypoint 1 With the User Waypoint Information Page displayed press the FMS knob to activate the Cursor 2 Turn the FMS knobs to enter a name for the new waypoint and press the ENT key The message Are you sure you want to create the new user waypoint is displayed With YES highlighted press the ENT key SECTION 8 FLIGHT PLANNING 3 Turn the large FMS knob to highlight the latitude longitude field or the Reference Way points field depending on how the waypoint is to be defined 4 Turn the FMS knobs to enter the position coordinates or the radial and distance from the reference waypoint 5 Press the ENT key to accept the new way point 6 Press the FMS knob to remove the flashing Cursor Create U
15. Press the Direct to G39 key 2 Turn the large FMS knob to highlight the Flight Plan Field or Nearest Airport Field 3 Turn the small FMS knob to display a list way points or airports Garmin G1000 Cockpit Reference Guide for the DA42 7 1 SECTION 7 NAVIGATION 4 Continue turning the small FMS knob to scroll through the list and highlight the desired waypoint or airport Press the ENT key to contirm the selection Press ENT again to activate a Direct to To re center the CDI HSI needle to the same destination waypoint fe Press the Direct to key followed by pressing the ENT key twice NOTE If a missed approach point MAP is the current destina tion the approach will be canceled To manually define the Direct to course 1 2 Press the Direct to 24 key Turn the FMS knobs to select the destination waypoint Press the ENT key to contirm the selected way point then turn the large FMS knob to highlight the Direct to Course field Turn the FMS knobs to select the desired course and press the ENT key Press the ENT key again to begin navigation using the selected destination and course Canceling Direct to Navigation 1 2 7 2 Press the Direct to G2 key Press the MENU key to display the Direct to options menu With Cancel Direct To NAV highlighted press the ENT key If a flight plan is still active the G1000 resumes navigating the flight plan along the closest l
16. Selection 0 c c600 5 2 5 4 Intercom System ICS Isolation 5 3 5 5 Intercom Squelch Control 5 3 5 6 Digital Clearance Recorder with Playback Capability ico2ce nconsccasneeins xtreme ands 5 4 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 1 SECTION 7 NAVIGATION 7 1 7 4 Navigation Map Page 7 1 Select the MAP Page Group 7 1 7 2 Direct to Navigation 7 1 Direct to Navigation from the MFD 7 1 Direct to Navigation from the PFD s 7 2 7 3 Airport Information 1 3 Select the Airport Information Page 7 3 Enter a Waypoint Facility Name or City Location 1 3 Access Runway Information 1 3 Access Frequency Information 1 3 7 4 Intersection Information 7 4 Select the Intersection Information Page ss11111111 7 4 Access Information on an Intersection c seseseeseerees 1 4 7 5 NDB Information 7 4 Select the NDB Information Page 7 4 View Information on a Specific NDB s s 7 4 7 6 VOR Information 7 5 Select the VOR Information Page c ssesesseesesseeseen 7 5 Access Information on a VOR 129 7 7 User Waypoint Information Page 7 5 7 8 Nearest Airports oo cesses esses 7 5 Nearest Airport Information on the MFD ssssssssssreees 7 5 Nearest Airports Information on the PFD 1 6 Garmin G1000 Cockpit Reference Guide for the DA42 TABLE OF CONTENTS 7 9 Neare
17. by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74A Air Data Computer or other altimeters in aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING The Jeppesen database used in the G1000 system must be updated regularly in order to ensure that its information remains current Updates are released every 28 days A database information packet is included in the G1000 package Pilots using an outdated database do so entirely at their own risk WARNING The basemap land and water data must not be used for navigation but rather only for non navi gational situational awareness Any basemap indication should be compared with other navigation sources WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING Use of the Stormscope interface for hazardous weather penetration thunderstorm penetration is prohibited Weather information on the G1000 MFD is approved only for weather avoidance not penetra tion WARNING Use of the GDL 69 Weather Interface for hazardous weather penetration is prohibited Weather information pro
18. displayed in the Traffic mode field 4 Press the STANDBY softkey to place the system in the Standby mode TIS STANDBY will be displayed in the Traffic mode field 5 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area If data is not received for a period longer than 6 sec onds the age of the present data will be displayed in the lower left of of the screen along with the annuciation that the system has entered Coast mode The system will maintain the traffic display up to 60 seconds until the next data reception If no data is received after 60 sec onds traffic will be removed from the display SECTION 10 HAZARD AVOIDANCE Traffic Advisory aircraft is 400 above amp Traffic out o Traffic Mode descending moving in the direction of the line o j Last data update Proximity Traffic at same Traffic 1600 above amp is older than 6 altitude level flight amp moving climbing moving in the sec resulting in in the direction of the line direction of the line Coast mode Figure 10 11 Traffic Map Page 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 TIS Audio Alert When a Traffic Advisory TA is displayed an audio alert Traffic is given Traffic Not Available will be heard wheneve
19. press the ENT key The departure will be active when the flight plan is active Load and Activate An Arrival Procedure 1 With the Navigation Map Page displayed press the FPL key 2 Press the LD STAR softkey If a flight plan is active the destination airport will be displayed as the default A list of available arrivals is also displayed 3 If no flight plan is active use the FMS knobs to enter the identifier of the desired airport Press the ENT key 4 Turnthe large FMS knob to highlight the Arrival field Turn the small FMS knob to display a list of available arrivals 5 Turn either FMS knob to select the desired arrival and press the ENT key Figure 9 3 Select Arrival Garmin G1000 Cockpit Reference Guide for the DA42 9 1 SECTION 9 PROCEDURES 6 A second window is displayed listing available 9 2 APPROACHES transitions for the arrival Turn either FMS knob to highlight the desired transition waypoint and Load and or Activate an Approach Procedure press the ENT key 1 With the Navigation Map Page displayed press the FPL key 2 Press the LD APR softkey If a flight plan is active the destination airport will be displayed as the default A list of available approaches is also displayed vrs 3 If no flight plan is active use the FMS knobs to Figure 9 4 Select Arrival Transition enter the identifier of the desired airport Press the ENT key 7 A third window is displayed listing the avail 4
20. the PROC key 2 Turn the large FMS knob to highlight ACTIVATE APPROACH 3 Press the ENT key The approach procedure is now active Garmin G1000 Cockpit Reference Guide for the DA42 9 3 SECTION 9 PROCEDURES This page intentionally left blank 9 4 Garmin G1000 Cockpit Reference Guide for the DA42 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 cursor flashes on the Map Setup option 2 Press the ENT key The Map Setup Menu is displayed Turn the small FMS knob to select the Weather or Traffic group to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS knob to return to the Navigation Map Page PAGE HENU OPTIONS Hop Setup Measure Bearing Distance Press the FMS CRSA knob to return to bose poge Figure 10 1 Page Menu HAP SETUP STRHSCP LTNG n STRHSCP HODE Ce STRMSCP SHEL SD NH NEXRAD DATA OFF 200ANH WH LTHG OFF 200GNH CELL MOVEMENT On Figure 10 2 Map Setup Menu MAP SETUP GROUP rete FFT Figure 10 3 Map Setup Group List TOPO TERRAIN SECTION 10 HAZARD AVOIDANCE 10 2 STORMSCOPE OPTIONAL WARNING Use of the Stormscope system for hazardous thunderstorm penetration is prohib ited Weather info
21. 4 4 Garmin G1000 Cockpit Reference Guide for the DA42 4 7 TRANSPONDER Mode Selection The STBY ON and ALT softkeys can be accessed by pressing the XPDR softkey Ground Mode Automatic GND is displayed when the aircraft is on the ground ENT EUX MIS Figure 4 11 Ground Mode Reply Status When the transponder sends replies to interrogations an R indication appears momentarily in the reply status field Figure 4 12 Reply Indication Code Selection 1 Press the XPDR softkey to display the transpon der Mode Selection softkeys 2 Press the CODE softkey to display the transpon der Code Selection softkeys which includes the digit softkeys 3 Press the appropriate digit softkeys to enter the code in the four digit code field of the Transponder Status bar Five seconds after the fourth digit has been entered the transponder code becomes activated When entering a code press the BKSP softkey as needed to back up and change code digits SECTION 4 NAV COM amp TRANSPONDER Following is a list of important codes e 1200 VER code in the U S please refer to the ICAO standards for VFR codes in other countries e 7000 VFR code commonly used in Europe please refer to the ICAO standards e 7500 Hijack code e 7600 Loss of communication code e 7700 Emergency code e 77 77 Military interceptor operations code NEVER ENTER THIS CODE e 0000 Code for military use in th
22. 77 AHRS GEA 71 Engine FUEL FLOW OR Airframe Unit s GMU 44 GIA 63 Integrated etai Sm Magnetometer Avionics Onit Lune OR a i OIL PRES BCU COOLANT TEMP gt o4 FUEL TEMP GIA 63 Integrated Avionics Units FUEL QTY GAL A WwW 1 7 Yt ENGINE a OBS CDI ADF DME XPD IDENT TMREREF NRST ALERTS GDC 74A Air Data GIA 63s OR GTX 33 Transponder Computer DME ADF Source OR GIA 63 Integrated Avionics Units Figure 12 5 G1000 System Failure Annunciations 12 4 G1000 SYSTEM MESSAGE ADVISORIES A NOTE This Section provides information regard This section describes various G1000 system message ing G1000 message advisories that may be dis advisories for the DA42 Certain messages are issued due played by the system Knowledge of the alrcr aft to an LRU or an LRU function failure Such messages are systems fl t conditions a sie varie normally accompanied by a corresponding red X annun ERel alo man PHONES THe De CONSE a WAEN B responding to a message Always use sound ciation as shown previously in the G1000 System Annun pilot judgment The Aircraft Flight Manual takes ciation section precedence over any conflicting guidance found in this section Garmin G1000 Cockpit Reference Guide for the DA42 12 7 SECTION 12 ANNUNCIATIONS amp ALERTS MFD amp PFD Message Advisories Message Comments S O DATA LOST Pilot stored data was The pilot profile data was lost System reverts to default pilot prof
23. ANCE Displaying Weather on the Weather Data Link 10 4 Page To select the Weather Data Link Page 1 Turn the large FMS knob to select the Map Page Group Turn the small FMS knob to select the Weather Data Link Page Press the available softkeys to select the desired XM weather product Press the LEGEND softkey to view the legends for the selected products If necessary turn either FMS knob to scroll through the list Press the small FMS knob or the ENT softkey to return to the map Figure 10 9 Weather Data Link Page NEXRAD press the NEXRAD softkey to show NEXRAD weather and radar coverage information Areas where radar coverage is not available will be shown in grayish purple The display is updated every five minutes NEXRAD Limitations Certain limitations exist regarding the NEXRAD radar displays Some but not all are listed here NEXRAD base reflectivity does not provide suf ficient information to determine cloud layers or precipitation characteristics hail vs rain etc e An individual NEXRAD site cannot depict high alti tude storms at close ranges and has no information about storms directly over the site The resolution of displayed NEXRAD data is 2 kilo meters Therefore when zoomed in on the display each square block is 2 kilometers The intensity level reflected by the square will be the highest level sampled within the 2 kilometer square area ECHO TOP press the ECHO TOP softke
24. BARO or BACK softkeys metric values to standard to return to the top level softkeys Figure 1 4 PFD Softkey Flow Chart 2 optional n noun an Press the BACK softkey to return to the top level softkeys softkey to return to the top level softkeys Press the BACK Figure 1 5 PFD Softkey Flow Chart 3 DOC OC 0 C0 CS ee ee n wn ns 1 6 Garmin G1000 Cockpit Reference Guide for the DA42 1 3 MFD SOFTKEYS ENGINE Pressing this softkey makes available the SYSTEM and FUEL softkeys which in turn access the System Page and the Fuel Page respectively MAP pressing this softkey enables the following softkeys TRAFFIC pressing this softkey displays removes Traffic on the Navigation Map TOPO pressing this softkey displays or removes topographic information on the Navigation Map TERRAIN pressing this softkey displays removes terrain and obstacle data on the Navigation Map A Press the BACK softkey on this level to return to the top softkey level nnn 4 Press the BACK softkey on this level to return to the top softkey level GH DO DnD AnD Ani D Figure 1 6 MFD Softkeys 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 Navigation Map XM LING optional pressing this softkey displays removes XM Radio lightnin
25. COM2 also becomes selected when the COM MIC key is pressed To prevent deselecting the desired received audio when pressing another COM MIC key press the already selected COMI or COM2 key before pressing the other COM MIC key COM MIC COM1 gt wv COM2 Figure 5 2 Transceivers 5 2 MARKER BEACON RECEIVER The marker beacon receiver is always ON Figure 5 3 shows the marker beacon annunciators on the PFD Inner Marker Annunciator Middle Marker Annunciator Marker Beacon Signal Sensitivity The HI SENS key can be pressed for increased marker beacon signal sensitivity il ll MKR HI SENS MUTE Figure 5 4 Marker Beacon 5 3 NAVIGATION RADIO SELECTION Pressing DME ADF NAVI or NAV2 selects and deselects the radio source and activates the annuncia tor Selected audio can be heard over the headset and the speakers These four keys can be selected individually or together Outer Marker Annunciator Figure 5 3 Marker Beacon Signal Indicator Lights on the PFD When the MKR MUTE key is pressed the key an nunciator is lit and the audio tone can be heard over the speaker or headsets during marker reception When the tone is active pressing the MKR MUTE key mutes the audio but does not affect the annunciator The audio returns when the next marker signal is received Garmin G1000 Cockpit Reference Guide for the DA42 lection scenarios are addressed in Table 5 1 SECTION 5 AUDIO PANE
26. FLTS Press to reset default settings on the PFD DME optional Press to display the DME informa tion window BRG bearing Press to cycle through the follow ing information NAV Displays NAV1 waypoint frequency or identifier and DME information in the BRG1 information window GPS Displays GPS waypoint identifier and GPS distance information in the BRG1 information window ADF Displays ADF waypoint frequency in the BRG1 information window OFF Removes the BRGI information window 360 HSI Press to display the 360 compass rose ARC HSI Press to display the 140 viewable arc BRG2 bearing Press to cycle through the follow ing information NAV2 Displays NAV2 waypoint frequency or identifier and DME information in the BRG2 information window GPS Displays GPS waypoint identifier and GPS distance information in the BRG2 information window ADF Displays ADF waypoint frequency in the BRG2 information window OFF Removes the BRG2 information window 1 4 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 1 SYSTEM OVERVIEW STD BARO Press to set the barometric pressure CODE Press to display transponder code selection to 29 92 inches of mercury 1013 hPa by softkeys 0 7 pressing the METRIC softkey 0 through 7 Press numbers to enter code BACK Press to return to the previous level IDENT Press to provide special aircraft position softkeys identification to Air Traff
27. Information Page Options or press the DELETE softkey 2 Turn the large FMS knob to select Delete User Waypoint and press the ENT key The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT key l 8 2 VIEWING THE ACTIVE FLIGHT PLAN Figure 8 4 Flight Plan Catalog Page 1 Press the FPL key 2 Press the FMS knob to activate the cursor 3 Turn the large FMS knob to highlight the desired flight plan and press the ACTIVE softkey 4 With OK highlighted press the ENT key to activate the flight plan To cancel the flight plan activation 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 large FMS knob to highlight the desired destination Figure 8 2 Active Flight Plan Page on the MFD waypoint 8 2 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 8 FLIGHT PLANNING 2 Press the ACT LEG softkey using MFD only 8 6 INVERT ACTIVE FLIGHT PLAN OR 3 Press the MENU key select the Activate Leg MENU key to display the Page Menu option from the page menu and press the ENT re key This step must be used when activating a 2 Turn the large FMS knob to highlight Invert leg from the PFD Flight Plan and press the ENT key The origi nal flight plan remains intact in its flight plan catalog storage lo
28. L x gt 5 5 INTERCOM SQUELCH CONTROL DME MAVI Select manual squelch for intercom audio by pressing the MAN SQ key to light the annunciator Pressing the small VOL SQ knob now toggles be tween volume and squelch adjustment by lighting VOL or SQ respectively Figure 5 5 Navigation Radios 5 4 INTERCOM SYSTEM ICS ISOLATION w MAN Press the PILOT and or COPLT key to select who is SQ PLAY isolated from hearing the Nav Com radios and music Se w CREW v PILOT COPLT ICS ISOLATION PILOT O PASS nl D d PILOT COPLT ICS ISOLATION Figure 5 6 ICS Isolation Figure 5 7 Volume Squelch Control PILOT KEY COPLT KEY Pilot Hears Conilot Hears Passenger ANNUNCIATOR ANNUNCIATOR p Hears Selected radios Selected radios Selected radios pilot copilot pilot copilot pilot copilot passengers passengers passengers MUSIC 1 MUSIC 1 MUSIC 2 OFF Copilot Copilot Selected radios passengers passengers pilot MUSIC 1 MUSIC 2 Selected radios Selected radios COPILOT pilot passengers Copilot pilot passengers MUSIC 1 MUSIC 2 ON Selected radios Selected radios Passengers pilot copilot pilot copilot MUSIC 2 Table 5 1 ICS Isolation Modes Garmin G1000 Cockpit Reference Guide for the DA42 5 3 SECTION 5 AUDIO PANEL 5 6 DIGITAL CLEARANCE RECORDER WITH PLAYBACK CAPABILITY Each reception of primary active COM audio is auto matically recorded in a memory block When the
29. Message Advisories 12 7 MFD amp PFD Message Advisories 12 8 Database Message Advisories 12 9 GMA 1347 Message Advisories s s s 12 10 GIA 63 Message Advisories ccsscesstesseesseeseesesseeen 12 11 GEA 71 Message Advisories scescesceseeseesteeseesean 12 13 GTX 33 Message Advisories 12 13 GRS 77 Message Advisories 12 14 GMU 44 Message Advisories cescecscestesseestesseeseen 12 14 GDC 74A Message Advisories 12 15 Miscellaneous Message Advisories 12 15 Index Index 1 Garmin G1000 Cockpit Reference Guide for the DA42 i TABLE OF CONTENTS This page intentionally left blank IV Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 1 SYSTEM OVERVIEW SECTION 1 SYSTEM OVERVIEW This guide gives the pilot abbreviated operating in structions for the Primary Flight Display PFD Multi The purpose of this Cockpit Reference Guide is to Function Display MFD and the GMA 1347 Audio Panel provide the pilot a resource with which to find operat System ing instructions on the major features of the G1000 ee system more easily It is not intended to be a A NOTE The pilot should read and thoroughly comprehensive operating guide Complete operat understand the Aircraft Flight Manual AFM for limitations procedures and operational infor mation not contained in this Cockpit Reference Guide The Aircra
30. Push the FMS knob to return to the Navigation Map Page To clear Stormscope lightning data from the Navigation Map Page i Press the MENU key with the Navigation Map Page displayed Turn either FMS knob to highlight the Clear Lightning Data field and press the ENT key Stormscope Page l 10 2 Turn the large FMS knob until the Map Page group is selected 2 Turn the small FMS knob until the Stormscope Page is selected 136 975 COM STRIKE RATE a Figure 10 6 Stormscope Page To change the Stormscope lightning mode between cell and strike 1 2 Select the Stormscope Page Press the MODE softkey The CELL and STRIKE softkeys are displayed Press the CELL softkey to display CELL data or press the STRIKE soft key to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells To change the viewing mode between 360 1 2 and 120 Select the Stormscope Page Press the VIEW softkey The 360 and ARC soft Garmin G1000 Cockpit Reference Guide for the DA42 keys are displayed Press the 360 softkey to display a 360 viewing are or press the ARC softkey to display a 120 viewing area Press the CLEAR softkey to remove all Storm scope lightning data from the display XM WEATHE
31. R OPTIONAL 10 3 WARNING Use of XM weather for hazard ous weather penetration is not recommended Weather information provided by XM Radio Service is approved only for weather avoidance not penetration 1 Press the MAP softkey 2 Press the NEXRAD or XM LTNG softkey to dis play the desired weather Press the applicable softkey again to remove weather data from the Navigation Map Page 136 975 AOD cer TNHEAP OL NORTH UP Se PLETOI ITS Cra T EI T ti L M TOPO TERRAIN Figure 10 7 Navigation Map Page Displaying NEXRAD Weather SECTION 10 HAZARD AVOIDANCE Displaying METAR and TAF information on the Airport Information Page To display METAR and TAF text on the Air port Information Page 1 Turn the large FMS knob to select the WPT Page Group 2 Turn the small FMS knob to select the Airport Information Page 3 Press the WX softkey to display METAR and TAF text METAR and TAF intormation is updated every 12 minutes SST eT alee lt lt lt MU KMSP PUBLIC MINNEAPOLIS ST PAUL INTL MINNEAPOLIS MN _ METAR Text 26000FT BROKEN TEMPERATURE 23 C DEW POINT 14 c ALTIMETER 29 721N IE FT_KMSP 2619452 1262 i GSH VC a5 2B ie 5 ag me TAF FH GSH Text VC BK J000 WX Ee Sole Figure 10 8 METAR and TAF Text Displayed on the Airport Weather Information Page Garmin G1000 Cockpit Reference Guide for the DA42 10 3 SECTION 10 HAZARD AVOID
32. RTS day f dE 4 INFORMATION rs i T i 8 Figure 7 8 VOR Information Page A Select the VOR Information Page 1 Turn the large FMS knob to select the WPT page Qrou D HAP RAWY FREQ APR 2 Turn the small FMS knob to select the fourth Figure 7 9 Nearest Airports Page rectangular page icon Nearest Airport Information on the MFD Access Information on a VOR Select the Nearest Airports Page 1 With the VOR Information Page displayed press 1 Turn the large FMS knob to select the NRST the FMS knob to activate the cursor page group 2 Turn the large FMS knob to highlight the 2 Turn the small FMS knob to select the first desired selection field identifier name or clos rectangular page icon est city Access Information on a Specific Airport 3 Turn the FMS knobs to enter an identifier name 1 Press the APT softkey located at the bottom or city and press the ENT key of the display The first airport in the nearest 4 Press the FMS knob to remove the flashing airports list is highlighted cursor 2 Turn the large FMS knob to highlight the desired airport Garmin G1000 Cockpit Reference Guide for the DA42 7 5 SECTION 7 NAVIGATION Access Runway Information for the 2 Press the ENT key to display airport informa Selected Airport tion 1 Press the RNWY softkey located at the bottom 3 Press the ENT key again cursor is on BACK of the display to return to the list 2 Turn the small FMS kno
33. Rs or SIGMETs Press the ENT key to display pertinent information for the selected product Note that pressing the ENT key when pan ning 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 display more information but allows the user to press the ENT key and select that Airport s Information Page to display the text of the report Pressing the ENT key when panning over a TFR displays TFR specific information Weather Products and Symbols Figure 10 10 depicts the symbol for each weather product read from left to right When a weather prod uct is active the product symbol is displayed in the lower right of the screen NEXRAD e Cloud Top Echo Top e XM Lightning e Cell Movement SIGMETS AIRMETS e METARs e City Forecast Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 10 HAZARD AVOIDANCE 10 6 e Surface Analysis Freezing Levels e Winds Aloft e County Warnings e Cyclone Warnings Echo Top Cloud Top and Echo Top Mutually Exclusive Figure 10 10 Weather Product Symbols The XM Information Page in the AUX Page Group will display the weather products available for the current sub scription green box by the weather product means that it is available NOTE The DONE softkey on the AUX XM INFOR MATION page is used to save the GDL 69 A acti vation data when the XM services are initial
34. 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 softkey makes available the SYSTEM and FUEL softkeys which in turn provide ac cess to the System Page and the Fuel Page respectively Engine Load Soe Indicator a0 6a 40 20 79 Loapz 78 3008 PT Tachometer 1800 1200 gaa 2330 RPM 2330 FUEL FLOW Fuel Flow Sien Maal TS on 4 Indicator OIL TEMP AE Oil Temperature Indicator OIL PRES Oil Pressure Indicator PR COOLANT TEMP Gar m jf Temperature Indicator Fuel FUEL TEMP Temperature Sa Indicator FUEL QTY GAL NA DE Fuel Quantity Indicator 8 53 16 15 2446 25 Figure 3 1 DA42 ENGINE Page SECTION 3 ENGINE INDICATION SYSTEM EIS 3 2 FUEL DISPLAY Engine Load S Indicator en 40 rai 72 LoD 72 3000 2400 B 1800 1200 686 2280 RPH 2280 l Fuel ____ Quantity 24 GAL Indicator GPH Fuel Temperature Indicator Gallons T s N Used ENDUR 94 52 Range in Nautical Seke a ee Miles TTL TIME IN SVC OHHOH HRS Figure 3 2 DA42 FUEL Page Tachometer Fuel Flow Indicator Gallons Remaining Endurance Total Time In Service Indicator If desired use the DEC FUEL INC FUEL and RST FUEL softkeys to adjust the amount of fuel remai
35. TRANSPONDER Standby NAV Selected NAV Selected COM Standby COM Frequency Field Frequency Navigation Status Window Frequency Frequency Field 60 110 60 _cky WPT VOR INFORMATION cx WT VORTNFORMATIN 118 400 Figure 4 2 Frequency Fields Tuning Box Active NAV Active COM Tuning Box Frequency Field Frequency Field 139 180 coM1 121 980 conz Frequency Toggle Arrow Tuning Box Figure 4 3 Frequency Toggle Arrow and Tuning Box NAV Controls COM Controls VOL PUSH VOL PUSH ID Knob SQ Knob Frequency Toggle Key Dual NAV Dual COM Knob Knob Turn to tune in desired frequencies e Press to change tuning box positions Figure 4 4 NAV COM Controls 4 2 Garmin G1000 Cockpit Reference Guide for the DA42 4 1 RADIO STATUS INDICATIONS e TX When a COM radio is keyed a white TX indication appears to the right of the corresponding COM frequency ID When the Morse code identifier is ON for a NAV radio a white ID indication appears to the lett of the corresponding active NAV frequency The Morse code identifier can be heard if the correspond ing NAV radio is selected on the audio panel COM TX COM2 121 900 Figure 4 5 Radio Status Indications 4 2 VOLUME VOLUME is displayed in place of the associated radio name i e COMI or NAV2 for two seconds after the volume level is last changed COM1 135 6 79 35 VOLUME Figure 4 6 COM Volume Level 4 3 AUTOMATIC SQUELCH Automatic squel
36. Traffic Annunciation 71 Alerts Window 2 Selected Heading Box Selected Course Box G Inset Map C Annunciation Window 4 BRGI Information Window Vertical Deviation Glideslope Indicator DME Information Window 1 Marker Beacon Annunciation 6 BRG2 Information Window Figure 2 2 Additional PFD Information Desired Track to Next Waypoint Distance to Next Waypoint Next Waypoint Current Track Figure 2 3 PFD Navigation Status Window default 2 2 Garmin G1000 Cockpit Reference Guide for the DA42 2 1 AIRSPEED INDICATOR Airspeed Trend ector Vyse Blue Line Vspeed References Vic Red Line Actual Airspeed Speed Ranges True Airspeed Box SEEN Figure 2 4 Airspeed Indicator Speed Indication The indicated airspeed is displayed inside the black pointer The pointer will become red upon reaching Vne Figure 2 5 Red Pointer at Vne Speed Ranges The color coded speed range strip denotes flaps op erating range normal operating range and never exceed speed Vne A red range is also present for low speed awareness Refer to the Airplane Flight Manual AFM for airspeed limitations and indicator markings Airspeed Trend Vector The end of the trend vector displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration deceleration is maintained SECTION 2 FLIGHT INSTRUMENTS Vspeed References Vspeed References are turned on or off in the Timer Refere
37. Turn the large FMS knob to highlight the able runways Turn the FMS knobs to select Approach field Turn the small FMS knob to the desired runway and press the ENT key display a list of available approaches Figure 9 5 Select Arrival Runway 8 With LOAD highlighted press the ENT key If a flight plan is active the selected arrival procedure is inserted after the destination Figure 9 6 Selecting an Approach Procedure airport and becomes part of the active flight plan If no flight plan is active when the arrival 5 Turn the FMS knobs to highlight the desired is loaded the arrival procedure will become the approach Press the ENT key active flight plan 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 final course segment of the approach and will provide navigation guidance relative to the final approach course 9 2 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 9 PROCEDURES Figure 9 7 Selecting an Approach Transition 7 Turn the large FMS knob to highlight Activate and press the ENT key to activate the approach Selecting Load will add the procedure to the flight plan without immediately using it for navigation guidance Activate An Approach in the Active Flight Plan 1 With the Navigation Map Page displayed press
38. adio for which the tuning failure was detected In the event of a dual display failure the emergency frequency 121 500 MHz automatically becomes the active frequency to the pilot through the pilot headset 11 3 UNUSUAL ATTITUDES The PFD will declutter when the aircraft enters an un usual attitude Only the basic primary functions will be displayed in these situations Red extreme pitch warning chevrons pointing toward the horizon are displayed starting at 50 degrees above and 30 degrees below the horizon line Figure 11 2 Extreme Pitch Indication 11 4 STORMSCOPE OPERATION WITH LOSS OF HEADING INPUT It heading is lost strikes and or cells must be cleared manually after the execution of each turn This is to en sure that the strike and or cell positions are depicted ac curately in relation to the nose of the aircraft 11 2 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 12 ANNUNCIATIONS amp ALERTS SECTION 12 ANNUNCIATIONS ALERTS Softkey Annunciation When the Alert ing System issues an alert the ALERTS softkey is AND ALERTS used as a flashing annunciation to accompany an alert During the alert the ALERTS softkey assumes a new label consistent with alert level WARNING A NOTE The Airplane Flight Manual Supplement CAUTION or ADVISORY Pressing the softkey supersedes information found in this docu ment annunciation acknowledges that the pilot is aware of the alert T
39. ansponder Status bar 4 5 Tropical storms 10 5 Turn rate indicator 2 6 TX 4 3 V Vertical Deviation Glideslope indica tor 2 4 VFR code 4 5 VHF 4 1 Voice alerts 12 5 VOL PUSH ID 4 2 VOL PUSH SQ 4 2 4 3 Volume squelch 5 3 Vspeeds 2 3 W WARN 2 7 Warning 12 1 12 2 Weather data link page 10 4 Weather product symbol 10 5 Weather product symbols 10 6 Weather warnings 10 5 Wind direction 10 5 Wind speed 10 5 X XM weather 10 3 10 4 XPDR softkey 4 5 Garmin G1000 Cockpit Reference Guide for the DA42 GARMIN At ns gt aa lt 2004 2005 Garmin Ltd or its subsidiaries Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A p 913 397 8200 f 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A p 503 391 3411 f 503 364 2138 Garmin Europe Ltd Unit 5 The Quadrangle Abbey Park Industrial Estate Romsey S051 9DL U K p 44 0870 8501241 f 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 www garmin com 190 00406 03 Rev B
40. ation Window Window Figure 2 14 HSI with Bearing Information Distance to Bearing Source Waypoint Identifier Ek Bearing Pointer Source Icon Figure 2 15 BRG1 Information Window Distance to Bearing Source EXT BUMI gt NAV Pointer Bearing Icon Source Figure 2 16 BRG2 Information Window Waypoint Identifier Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 2 FLIGHT INSTRUMENTS DME Radio optional To display the DME Information Window press the PFD softkey followed by the DME softkey Figure 2 17 DME Information Window Navigation Source To change between navigation sources 1 Press the CDI softkey to change trom GPS to VOR1 LOC1 2 Press the CDI softkey again to change from VOR1 LOC1 to VOR2 LOC2 3 Press the CDI softkey a third time to return to GPS e INTEG RAIM is not available Figure 2 18 GPS INTEG GPS SUSP LOC1 and VOR2 e WARN GPS detects a position error To enable disable OBS mode while navigating with GPS 1 Press the OBS softkey to select OBS Mode 2 Turn the CRS knob to select the desired course TO FROM the waypoint 3 Press the OBS softkey again to return to normal operation A NOTE The OBS softkey is only displayed when navigating an active leg Garmin G1000 Cockpit Reference Guide for the DA42 2 7 SECTION 2 FLIGHT INSTRUMENTS This page intentionally left blank 2 8 Garmin G1000 Cockpit Reference Guide for the DA42
41. b to select the desired Load an Airport COM Frequency into the runway Active COM Quickly Tune the COM Transceiver to a 1 Turn the large FMS knob to place the cursor Nearby Airport Frequency on the desired airport frequency shown in the 1 Press the FREQ softkey located at the bottom nO of the display 2 Press the ENT key and the selected frequency will become the standby frequency for the 2 Turn either FMS knob to select the desired active COM frequency 3 Press the Frequency Toggle key to make the 3 Press the ENT key The selected frequency is frequency the active frequency placed in the standby frequency tuning box 4 Press the Frequency Toggle key to place the frequency in the active field Nearest Airports Information on the PFD Bearing 10 Distance Airport Symbol NEAREST AIRPORTS Identifier US RE KT VFR MULTICOM 122 900 RNWY 3500FT Runway Length KIDA 261 9 5NH ILS THF ORMAT ION TOWER 118 500 RNWY S O1FT KRXE 4 352 20 1nM VORI UNICOM 122 800 RNWY 420 FT N 46362 MIS LIT REFERENCE VOR KE 115 30 Primary COM Frequency Figure 7 10 Nearest Airports Window 1 Press the NRST softkey to display the PFD Near est Airports Window Figure 7 11 Nearest Intersections Page View Information on a Specific Airport in Select the Nearest Intersections Page the List 1 Turn the large FMS knob to place the cursor on 1 Turn the large FMS knob to select the NRST the desired airport i
42. been detected in the GPS1 and or GPS2 receiver The receiver is unavailable The G1000 system should be serviced A failure has been detected in the GPS1 and or GPS2 receiver The receiver may stil be available The G1000 system should be serviced A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G1000 system should be serviced The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transter switch again to cycle its operation If the problem persists the G1000 system should be serviced Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63 Message Advisories Cont Alerts Window Message Comments o G S1 FAIL G ST is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 G S2 FAIL G S2 is inoperative system should be serviced G S1 SERVICE G S1 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver G S2 SERVICE G S2 needs service may still be available The G1000 system should be serviced when possible Return unit for repair GEA 71 Message Advisories Alerts Window Message Comments S O GEA1 CONFIG GEA1 configuration The GEA 71 configuration settings do not match those of backup configuration error Contig service req d memory The G1000 sys
43. cation 3 With OK highlighted press the ENT key to invert the flight plan 1 From the Active Flight Plan Page press the 4 With Activate highlighted press the ENT key ACTIVATE M ne eo Figure 8 5 Activate Flight Plan Leg Confirmation 8 5 STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL key to display the Active Flight Plan Page 2 Press the MENU key to display the Page Menu window Figure 8 9 Invert Flight Plan Confirmation 8 7 CREATE NEW FLIGHT PLAN Figure 8 6 Delete Flight Plan To 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 3 Turn the large FMS knob to highlight Delete Flight Plan and press the ENT key With OK highlighted press the ENT key to deactivate the flight plan This will not delete the stored 2 Press the NEW softkey to display a blank flight flight plan only the active flight plan plan page for the first empty storage loca tion Figure 8 7 Delete Flight Plan Confirmation Garmin G1000 Cockpit Reference Guide for the DA42 8 3 SECTION 8 FLIGHT PLANNING STORED FLIGHT PLAN Figure 8 10 Create FPL on MFD 3 Turn the small FMS knob to display the Way point Information Page Turn the small FMS knob to enter the first character of the identifier of the departure waypoint Turn the large FMS knob to move the cursor to the next character field Repeat using the
44. ch can be disabled for a COM radio by pressing the COM knob to select the desired COM sub window then by pressing the VOL PUSH SQ knob 4 4 QUICKLY ACTIVATING 121 500 MHZ Pressing and holding the COM Frequency Toggle key for approximately two 2 seconds automatically tunes the selected COM radio to the emergency frequency SECTION 4 NAV COM amp TRANSPONDER 4 5 OPTIONAL NAV RADIOS ADF Radio optional To tune the ADF 1 From the Tuning window turn the large FMS knob to highlight the ADF tuning field 2 Turn the small FMS knob to enter the first digit 3 Turn the large FMS knob to select the next desired digit field Turn the small FMS knob to again select the desired digit 4 When the desired frequency is entered press the ENT key to transter the frequency into the active field 5 Turn the large FMS knob to select the MODE field Turn the small FMS knob to select ADF or BFO 6 Turn the large FMS knob to select the volume field if desired Turn the small FMS knob to adjust the ADF volume to the desired level 7 Press the FMS knob to exit all the fields ADF DME TUNING Ai MODE 4 ADF gt VoL 5 Z DME MODE NAV ENT TO TRANSFER XPDR 1288 STBY LCL 16 52 54 ADF DME XPDR IDENT TMR REF NRST HARNING Figure 4 7 ADF DME Tuning Window Garmin G1000 Cockpit Reference Guide for the DA42 4 3 SECTION 4 NAV COM amp TRANSPONDER DME Radio optional 4 6 FREQUENCY AUTO TUNING The Tuning
45. cies Page selected press the ARTCC FSS or Wx softkey 2 Turn the large FMS knob to select the fre quency 3 Press the ENT key to load the frequency into the COM frequency standby field 1 14 NEAREST AIRSPACES NORTH UP Figure 7 16 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 seventh rectangular page icon Airspace Alerts Box Ifthe projected course takes the aircraft inside an airspace within the next ten minutes Ahead is SECTION 7 NAVIGATION displayed e Ifthe aircraft is within two nautical miles of an airspace and the current course takes the aircraft inside Ahead lt 2 nm is displayed e Ifthe aircraft is within two nautical miles of an airspace and the current course will not take the aircraft inside Within 2 nm is displayed e Ifthe aircraft has entered an airspace Inside is displayed View Additional Details for a Listed Airspace 1 Select the Nearest Airspace Page 2 Press the FMS knob to activate the cursor 3 Turn the large FMS knob to scroll through the list highlighting the desired airspace 4 Press the ALERTS softkey and turn either FMS knob to select the desired airspace 5 Press the FMS knob to remove the flashing Cursor View and Quickly Load the Frequency for a Controlling Agency 1 Select the Nearest Airspaces Page 2 Press the
46. craft is inside the airspace ARSPC AHEAD Airspace ahead less Special use airspace is ahead of aircraft The aircraft will penetrate the airspace than 10 minutes within 10 minutes than 2 nm not be smooth Prepare for steep turns ahead and expect noticeable course deviations active proach when required sequence mode deactivate the OBS mode SLCT FREQ Select appropriate The system notities the pilot to load the approach frequency for the appropriate NAV frequency tor approach receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for The system notities the pilot to set the CDI to the correct NAV receiver Set the CDI approach to the correct NAV receiver NO WGS84 WPT Non WGS 84 The selected waypoint xxxx does not use the WGS 84 datum Cross check position waypoint for navigation Xxxx with alternate navigation sources iia REA Rene The traffic information system TIS has failed The G1000 system should be serviced Eva a Stormscope has failed The G1000 system should be serviced BACKUP PATH Stormscope using Stormscope is using the backup communication path The G1000 system should be backup path serviced when possible 12 16 Garmin G1000 Cockpit Reference Guide for the DA42 A Abnormal COM operation 11 2 Activate a flight plan 8 2 Active flight plan 8 2 ADF 1 4 ADVISORY 12 1 Advisory alerts 12 4 Age 10 6 AHRS 12 14 Aircraft alerts 12 3 AIRMET 10 5 Airport frequency
47. d and IOCKEC played the pilot may use the large FMS knob to PITOT OFF Pitot heat is off scroll through the alert list Higher priority alerts are XPDR 1200 ALT LCL 00 46 53 displayed at the top of the window Lower priority ALERTS Softkey alerts are displayed at the bottom of the window Figure 12 1 G1000 Alerting System ue Garmin G1000 Cockpit Reference Guide for the DA42 12 1 SECTION 12 ANNUNCIATIONS amp ALERTS 12 1 ALERT LEVEL DEFINITIONS WARNING The G1000 Alerting System as installed in Diamond DA42 and DA42L aircraft uses three alert levels Figure 12 2 WARNING Softkey Annunciation e WARNING This level of alert requires immediate pilot attention A warning alert is accompanied by an annunciation in the Annunciation window Warning text appearing in the Annunciation window is RED A warning alert is also accompanied by a flashing WARNING softkey annunciation as shown bon I in Figure 12 2 Pressing the WARNING softkey Figure 12 3 CAUTION Softkey acknowledges the presence of the warning alert and Annunciation stops the aural tone if applicable e CAUTION This level of alert indicates the exis tence of abnormal conditions on the aircraft that may require pilot intervention A caution alert is accompanied by an annunciation in the Annun ADVISORY ciation window Caution text appearing in the DYI SURY Annunciation window is YELLOW A caution alert Figure 12 4 ADVISORY Softkey is also accompanied by a
48. database The PFD and MFD have different aviation database types installed Americas Euro type mismatch Xtalk is off pean etc Crosstill is off Install correct aviation database type in both displays DB MISMATCH Basemap database The PFD and MFD have different basemap database versions installed Crossfill is version mismatch Xtalk is off off Install correct basemap database version in both displays DB MISMATCH Terrain database The PFD and MFD have different terrain database versions installed Crossfill is off version mismatch Xtalk is off Install correct terrain database version in both displays DB MISMATCH Terrain database The PFD and MFD have different terrain database types installed Crossfill is off type mismatch Xtalk is off Install correct terrain database type in both displays DB MISMATCH Obstacle database The PFD and MFD have different obstacle database versions installed Crossfill is off version mismatch Xtalk is off Install correct obstacle database version in both displays Garmin G1000 Cockpit Reference Guide for the DA42 12 9 SECTION 12 ANNUNCIATIONS amp ALERTS GMA 1347 Message Advisories Alerts Window Message Comments S O GMA1 FAIL GMAT is inoperative The audio panel self test has detected a failure The audio panel is unavailable The G1000 system should be serviced GMA1 CONFIG GMA1 configuration The audio panel configuration settings do not match backup configuration
49. dentifier page group 7 6 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 7 NAVIGATION 2 Turn the small FMS knob to select the second on the Nearest NDB Page pertains to the rectangular page icon selected NDB View Information on the Nearest Intersection 711 NEAREST VOR 1 Press the FMS knob to activate the cursor Select the Nearest VOR Page 2 Turn either FMS knob to select the desired intersection Press the ENT key 1 Turn the large FMS knob to select the NRST page group 7 10 NEAREST NDB 2 Turn the small FMS knob to select the fourth rectangular page icon 1795 AU PC E S TOME Re eon Figure 7 12 Nearest NDB Page Figure 7 13 Nearest VOR Page Select the Nearest NDB Page 1 Turn the large FMS knob to select the NRST View Information on the Nearest VOR page group 1 With the Nearest VOR Page selected press the 2 Turn the small FMS knob to select the third VOR softkey rectangular page icon eee age 2 Turn the FMS knobs to select a VOR Press the Access Information on a Specific NDB ENT key OR Press the MENU key Select the Select VOR Window option and press the ENT key Turn either FMS knob to select a VOR 1 Press the FMS knob to activate the cursor 2 Turn either FMS knob to select the desired NDB Press the ENT key The remaining information Garmin G1000 Cockpit Reference Guide for the DA42 7 7 SECTION 7 NAVIGATION 1 8 Select and Load a VOR Frequency 1
50. e desired flight plan and press the ENT key 4 8 14 8 15 SECTION 8 FLIGHT PLANNING Turn the FMS knobs to make the desired changes then press the ENT key Press the FMS knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN Press the FPL key and turn the small FMS knob to display the Flight Plan Catalog Page Press the FMS knob to activate the cursor Turn the large FMS knob to highlight the desired flight plan and press the ENT key Turn the large FMS knob to select the waypoint to be deleted and press the CLR key to display a REMOVE WAYPOINT contirmation window With OK highlighted press the ENT key to remove the waypoint To cancel the delete request turn the large FMS knob to highlight CANCEL and press the ENT key Once all changes have been made press the FMS knob to return to the Flight Plan Page Remove KCRQ OK or CANCEL Figure 8 14 Remove Waypoint Confirmation INVERT AND ACTIVATE A STORED FLIGHT PLAN From the Flight Plan Catalog Page press the FMS knob to activate the cursor Turn the large FMS knob to highlight the desired flight plan and press the MENU key to display the Page Menu options Garmin G1000 Cockpit Reference Guide for the DA42 8 5 SECTION 8 FLIGHT PLANNING 3 Turn the large FMS knob to highlight Invert Flight Plan and press the ENT key The origi nal flight plan remains intact in its flight plan catal
51. e U S Flight ID Reporting If so configured the Flight ID may be entered in the Timer Reference window If configuration is set to SAME AS TAIL the aircraft tail number will always be dis played GLIDE Ur Vx Vy FLIGHT ID Flight ID Figure 4 13 Timer References Window Garmin G1000 Cockpit Reference Guide for the DA42 4 5 SECTION 4 NAV COM amp TRANSPONDER This page intentionally left blank 4 6 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 5 AUDIO PANEL B r B ai COM MIC B ai Transmitters COM3 MIC is unavailable Split COM Unavailable Passenger Address Marker Beacon Mute Aircraft Navigation Radio Audio ADF amp DME optional AUX T SECTION 5 AUDIO PANEL nn COMI Transceiver Audio COM 3 is unavailable Telephone Unavailable Speaker Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio unavailable Manual Squelch foo y Recorded COM Audio Playback CREW PILOT con ICS Isolation ICS ISOLATION PILOT QO PASS VOL SQ Volume Squelch VOL Annunciation SQ Annunciation Reversionary Mode DISPLAY BACKUP Figure 5 1 Audio Panel Controls Garmin G1000 Cockpit Reference Guide for the DA42 5 1 SECTION 5 AUDIO PANEL 5 1 COM RADIO SELECTION Pressing the COMI MIC or COM2 MIC key selects the active transmitter i e microphone The associated receiver audio COMI or
52. e by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations NOTE When using Stormscope there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode However clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the most current G1000 system Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation Garmin G1000 Cockpit Reference Guide for the DA42 W 3 WARNINGS CAUTIONS amp NOTES This page intentionally left blank W 4 Garmin G1000 Cockpit Reference Guide for the DA42 RECORD OF REVISIONS Part Number Change Summary 90 00406 00 Initial Release 1 190 00406 01 Added DME capability Added BRG1 BRG2 pointers Changed Airspeed Trend Vector Changed Altitude Tr
53. ed Press the ENT key when finished Garmin G1000 Cockpit Reference Guide for the DA42 8 SECTION 8 FLIGHT PLANNING This page intentionally left blank 8 8 Garmin G1000 Cockpit Reference Guide for the DA42 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 Ifa flight plan is active the departure airport will be displayed as the detault A list of available departures is also displayed 3 If no flight plan is active use the FMS knobs to enter the identifier of the desired airport Press the ENT key 4 Turn the large FMS knob to highlight the Depar ture field Turn the small FMS knob to display a list of available departures 5 Turn either FMS knob to select the desired departure and press the ENT key AIRPORT RTD LA PUBLIC HEH CENTURY AIRCENTER OLATHE KS DEPARTURE CHIEFS TIFT 02 M HLDCT2 Figure 9 1 Select Departure 6 A list of runways may be displayed for the departure Turn the FMS knobs to select the desired runway and press the ENT key 7 Alist of available transitions is displayed for the departure Turn either FMS knob to highlight the desired transition waypoint and press the ENT key SECTION 9 PROCEDURES DEPARTURE CHIEFS RUNWAY ALL TRANSITION CATTE Figure 9 2 Select Departure Transition 8 With LOAD highlighted
54. eg PAGE MENU OPTIONS Conceal Direct To NA Press the FMS CRSA knob to return to bose poge Figure 7 3 Canceling Direct to Navigation Direct to Navigation from the PFD WPT Symbol DIRECT TO Identifier JACKSON WY WPT Location Facility Name Flight Plan WPT Nearest WPT Bearing to WPT N 4336 44 Lat Lon Distance from WPT CIO Course to Selected WPT ACTIVATE Figure 7 4 PFD Direct to Window Press the Direct to key G2 Turn the large FMS knob to place the cursor in the desired selection field Turn the small FMS knob to begin selecting the desired identifier location etc Press the ENT key The cursor is now flashing on ACTIVATE Press the ENT key again to activate Cancelling Direct to Navigation 1 2 Press the Direct to 8 key Press the MENU key to display the Options Window The cursor will be flashing on Cancel Direct to NAV Press the ENT key to cancel the direct to Garmin G1000 Cockpit Reference Guide for the DA42 Figure 7 5 Airport Information Page Select the Airport Information Page 1 Turn the large FMS knob to select the WPT page group Turn the small FMS knob to select the first rectangular page icon Enter a Waypoint Facility Name or City Location 1 2 Press the FMS knob to activate the cursor Turn the large FMS knob to select the facility name or location city field Turn the small FMS knob to select the desired character
55. end Vector Added Checklist capability Added Flight ID capability 190 00406 02 Reformatted manual to new format Added deicing capability Updated Annunciations and Alerts 190 00406 03 Added XM Weather capability Added TAWS B Updated Message Advisories Added Lycoming engine parameters Revision at of Revision fected Pages 8 16 05 i Index 4 Initial Release 11 22 05 Copyright Page Changed System SW applicability to 0370 13 or later 1 7 Corrected Figure 1 6 Section 3 Removed all references to the DA42L Section 10 Removed all references to TAWs and the DA42L Section 12 Removed all references to the DA42L Garmin G1000 Cockpit Reference Guide for the DA42 RR 1 RECORD OF REVISIONS This page intentionally left blank RR 2 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 1 SYSTEM OVERVIEW 1 1 1 1 PFD MFD Controls 1 2 1 2 PFD Softk ys nent sn 1 4 1 3 MED SOTK CYS ones 1 7 1 4 MFD Page Groups 1 8 1 5 BACRIQNTNO Send dE 1 8 SECTION 2 FLIGHT INSTRUMENTS 10001100 2 1 2 1 Airspeed Indicator 2 3 Speed INGICAION ss 2 3 Speed Ranges nement 2 3 Airspeed Trend Vector 2 3 Vspeed References 2 3 2 2 Attitude Indicator 0 0 0 ccc 2 3 2 3 Altimeter 2 4 Altitude Reference Bug 2 4 Altitude Trend Vector 2 4 Barometric Setting BOX rennais ss 2 4 2 4 Vertical Deviation Glideslope I
56. er Waypoint cesssesssessssessessecsnessnesssesssen 8 2 8 2 Viewing the Active Flight Plan 8 2 8 3 Activate a Stored Flight Plan 8 2 8 4 Activate a Flight Plan Leg 0 8 2 8 5 Stop Navigating a Flight Plan 8 3 8 6 Invert Active Flight Plan 8 3 8 7 Create a New Flight Plan 8 3 8 8 Load a Departure occ 8 4 8 9 Load an Arrival 8 4 8 10 Load an Approach ccc 8 4 8 11 Remove a Departure Arrival or Approach from a Flight Plan 8 5 8 12 Store a Flight Plan 8 5 8 13 Edit a Stored Flight Plan 8 5 8 14 Delete a Waypoint from the Flight Plan 8 5 8 15 Invert and Activate a Stored Flight Plan 8 5 8 16 Copy a Flight Plan 8 6 8 17 Delete a Flight Plan 8 6 8 18 Graphical Flight Plan Creation 8 6 8 19 Trip Planning 8 6 SECTION 9 PROCEDURES 9 1 9 1 Arrivals and Departures 9 1 Load and Activate a Departure Procedure cscse 9 1 Load and Activate An Arrival Procedure 9 1 9 2 Approaches 2468 00 nn 9 2 Load and or Activate an Approach Procedure 9 2 Activate An Approach in the Active Flight Plan 9 3 SECTION 10 HAZARD AVOIDANCE 10 1 10 1 Customizing the Hazard Displays on the Navigation Map 10 1 10 2 STORMSCOPE Optional 0 0 0 10 1 Displaying Stormscope Lightning Data on the Navigation ADE PAG nee hoannas 10 1 OM COVE PaO et 10
57. flashing CAUTION softkey Annunciation annunciation as shown in Figure 12 3 Pressing the CAUTION softkey acknowledges the presence of the caution alert e MESSAGE ADVISORY This level of alert provides general information to the pilot A message advisory alert does not issue annunciations in the Annuncia tion window Instead message advisory alerts only issue a flashing ADVISORY softkey annunciation as shown in Figure 12 4 Pressing the ADVISORY softkey acknowledges the presence of the message advisory alert and displays the alert text message in the Alerts window 12 2 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 12 ANNUNCIATIONS amp 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 Alerts Continuous Aural Tone Autopilot automatic trim is inoperative CAUTION Alerts Single Aural Tone Pitot heat is off Stall warning heat has failed Pitot heat has failed Stall warning heat is off Left right auxiliary fuel tank is empty Garmin G1000 Cockpit Reference Guide for the DA42 12 3 SECTION 12 ANNUNCIATIONS amp ALERTS Annunciation Window Text Alerts Window Message Audio Alert De icing tluid level is low F JF J Single Aural Tone De icing pressure is low Stick limiting system has failed Annunciation Advisory Alerts Annunciation Wind
58. ft Flight Manual always takes e G1000 Primary Flight Display Pilots Guide precedence over the information found in this e G1000 VHF NAV COM Pilots Guide guide e G1000 Transponder Pilots Guide e G1000 GMA 1347 Audio Panel Pilots Guide e G1000 Engine Indication System Pilots Guide e G1000 Multi Function Display Pilots Guide e G1000 Optional Equipment Pilots Guide ing procedures for the complete system are found in the following documents Garmin G1000 Cockpit Reference Guide for the DA42 1 1 SECTION 1 SYSTEM OVERVIEW 1 1 PFD MFD CONTROLS s s PUSH VOL sQ lt gt 1 COM EMERG PUSH 1 2 CRS 2 BARO PUSH PUSH HDG SYNC CRS CTR RANGE Pee PUSH CRSR 17 Figure 1 1 PFD MFD Controls MENU FPL PROC CLR ENT DFLT lp F M S 0009 PUSH CASA 1 2 Garmin G1000 Cockpit Reference Guide for the DA42 1 NAV VOL ID Knob Controls the NAV audio level Press to toggle the Morse code identifier ON and OFF Volume level is shown in the field as a percentage 2 NAV Frequency Toggle Key Toggles the standby and active NAV frequencies 3 Dual NAV Knob Tunes the MHz large knob and kHz small knob standby frequencies for the NAV re ceiver Press to toggle the tuning cursor light blue box between the NAVI and NAV2 fields 4 Heading Knob Turn to manually select a heading on the HSI When pressed it synchronizes the heading bug wi
59. ftkey OFF optional Nnonnoonoonoaso Figure 1 2 PFD Top Level Softkeys INSET Press to display the Inset Map in the lower left corner of the PFD OFF Press to remove the Inset Map DCLTR 3 Press momentarily to select the desired amount of map detail The declutter level appears adjacent to the DCLTR softkey e No declutter All map features are visible Declutter 1 Declutters land data Declutter 2 Declutters land and SUA data Declutter 3 Declutters large NAV data remaining removes everything except the active flight plan TRAFFIC Press to display TIS traffic on the map TOPO Press to display topographical data i e coastlines terrain rivers lakes etc and elevation scale on the inset map TERRAIN Press to display terrain information on the inset map STRMSCP optional Press to display the light ning data on the inset map within a 200 nm radius of the aircraft NEXRAD optional Press to display NEXRAD precititation data on the inset map XM LING optional Press to display the XM Radio lightning data on the inset map BACK Press to return to the previous level softkey configuration PFD Press to display the additional softkeys for additional configurations to the PFD METRIC Press to display the current and refer ence altitudes in meters in addition to feet Pressing the metric softkey also changes the barometric setting to hectopascals D
60. g data on the Navigation Map BACK pressing this softkey displays the ENGINE and MAP top level softkeys DCLTR declutter pressing this softkey removes map information in three levels es optional Press to return to the top softkey level optional optional optional TOPO TERRAIN BACK AR AA AAA The DONE softkey changes to UNDO when the checklist item is already checked mas mn Garmin G1000 Cockpit Reference Guide for the DA42 1 7 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 Nearest Group Auxiliary Page Group Number of Pages in Current Waypoint Page Group Map Page Group Figure 1 7 Page Group Icon Selected Page 1 5 BACKLIGHTING PFD SETUP MENU To manually adjust the backlight for the PFD psPL gt EE 23 477 PFD and MFD i MFD DSPL AUTO o f 1 Press the MENU key on the PFD to display the PFD Setup Menu window 2 Press the small FMS knob to activate the cursor PFD DSPL gt AUTO is now high lighted 3 Turn the small FMS knob to display the Figure 1 8 PFD Setup Menu Window selection window 4 Turn the FMS knob to select MANUAL then press the ENT key 5 With the intensity value now highlighted turn the small FMS knob to select the desired backlighting 6 Turn the large FMS knob to hig
61. he FMS knobs to enter the identifier of the trom waypoint Once the waypoints identifier is entered press the ENT key to accept the waypoint The flashing cursor moves to the to waypoint Again turn the FMS knobs to enter the identi fier of the to waypoint and press the ENT key to accept the waypoint OR For flight plan leg planning press the FPL SECTION 8 FLIGHT PLANNING softkey at the bottom of the display and turn the small FMS knob to select the desired flight plan already stored in memory by number Turn the large FMS knob to highlight the LEG field and turn the small FMS knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan Turn the large FMS knob to highlight the depar ture time DEP TIME tield Turn the FMS knobs to enter the departure time Press the ENT key when finished Departure time may be entered in local or UTC time depending upon unit settings Turn the FMS knobs to enter the fuel flow Press the ENT key when finished Note that in automatic page mode fuel flow is provided by the system The flashing cursor moves to the fuel on board field Turn the FMS knobs to modify the fuel on board Press the ENT key when finished Note that in automatic mode this is provided by the system The flashing cursor moves to the calibrated airspeed field Turn the FMS knobs to enter an calibrated airspe
62. he MAP Page Group 1 TRAFFIC Turn the large FMS knob until MAP is high lighted in the page group window in the lower right of the MFD display Turn the small FMS knob to select the first MAP page indicated by a solid rectangular icon Press the MAP softkey to display softkeys for the available information which may be displayed on the map WARNING The map display should only be used for situational awareness Any map display indication should be compared with approved navigation sources Figure 7 1 Navigation Map Page SECTION 7 NAVIGATION 7 2 DIRECT TO NAVIGATION Direct to Navigation from the MFD DIRECT Ti Identifier NT DRE Symbol Facility Name MIAMI INTL City MIAMI FL Flight Plan Field gt mn ve Nearest Airport Map Orientation Map of the Selected Waypoint Map Range Bearing Region Distance Latitude Longitude Activate Field ourse Figure 7 2 MFD Direct to Window To enter a Direct to destination 1 Press the Direct to E39 key 2 Turn the small FMS knob to enter the first letter of the destination waypoint identifier Turn the large FMS knob to the right to move the cursor to the next character position 3 Repeat step 2 to spell out the rest of the way point identifier 4 Press the ENT key to confirm the identifier The Activate field is highlighted 5 Press the ENT key to activate To select a Direct to destination to a flight plan waypoint or nearest airport 1
63. he softkey then returns to the previ ous ALERTS label The pilot can then press the The G1000 Alerting System conveys alerts to the pilot ALERTS soitkey again to view alert text messages using a combination of the following items System Annunciations Typically a large red X appears in a window when a related LRU fails or detects invalid data e Annunciation Window The Annunciation window displays abbreviated annunciation text The Annunciation window is located to the right of the Altitude and Vertical Speed windows on the PFD display or the MFD if system is in reversionary mode Up to 12 annunciations can be displayed simultaneously A white horizontal line separates annunciations that are acknowledged from annun ciations that are not yet acknowledged Acknowl edged annunciations are always above the line eo Annuciations are displayed in order of priority from Red X top to bottom The highest priority annunciation is displayed at the top of the Annunciation Window o Annunciation e Alerts Window The Alerts window displays alert Wanao text messages Up to 64 prioritized alerts can be dis played in the Alerts window Pressing the ALERTS GDC1 FAIL GDC1 is inoperative softkey displays the Alerts window Pressing the ALTERNATOR Alternator failed ALERTS softkey again removes the Alerts window Py ie y Os ae jg Alerts Window from the display When the Alerts window is dis P ia ora oor is not ciose
64. he system notifies the pilot that the timer has expired DB CHANGE Database changed This occurs when a stored flight plan contains procedures that have been manually Verify user modified procedures edited This alert is issued only after an aviation database update Verity that the user moditied procedures in stored flight plans are correct and up to date FPL TRUNC Flight plan has been This occurs when a newly installed aviation database eliminates an obsolete ap truncated proach or arrival used by a stored flight plan The obsolete procedure is removed trom the flight plan Update flight plan with current arrival or approach APPR VPROF Approaching VNAV Aircraft is approaching VNAV profile Prepare to climb or descend to meet VNAV profile profile 2 OR AAC Aircraft is approaching target altitude Prepare to level aircratt Garmin G1000 Cockpit Reference Guide for the DA42 12 15 SECTION 12 ANNUNCIATIONS amp ALERTS Miscellaneous Message Advisories Cont Alerts Window Message Comments S LOCKED FPL Cannot navigate locked This occurs when the pilot attempts to activate a stored flight plan that contains flight plan locked waypoint Remove locked waypoint trom flight plan Update flight plan with current waypoint ae sn Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The air
65. hlight MFD DSPL gt AUTO and repeat steps 3 through 5 1 8 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 2 FLIGHT INSTRUMENTS SECTION 2 FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display unless otherwise indicated navi113 25 118 98 HF DIS RK 118 900 133 888 com NAVZ 118 98 124 306 COM 7 ronn Bail E 7000 Bone Rini ow 6760 Fs an Tini 6504 4 he Thi Ne STH Ti r ij PoE INSET FD CD NBS POR IDENT TMR REF NRST ALERTS H Li O NAV Frequency Window 0 Turn Rate Indicator Airspeed Indicator Barometric Setting Box G True Airspeed Box Vertical Speed Indicator Heading Box Altimeter 5 Horizontal Situation Indicator 13 Altitude Reference Box 6 Outside Air Temperature Box COM Frequency Window 7 System Time Box 15 Navigation Status Bar Transponder Status Bar Slip Skid Indicator Figure 2 1 Default PFD Information Garmin G1000 Cockpit Reference Guide for the DA42 2 1 SECTION 2 FLIGHT INSTRUMENTS navi 108 00 P TRE 136 975 118 000 com NAV 117 95 136 975 COH ALERTS RS CPs AHRS not receiving backup GPS information BACKUP PATH Airdoto using LT dato path BACKUP PATH AHRS using bockup bell path 1495 tt MOC o m URI ADE pron 1200 STEV tt 07 58 21 INSET FD COI ADF OME XPOR IDENT TMR REF NRST WARNING
66. ic Control ATC OBS Press to select OBS mode on the CDI when BKSP Press to remove numbers entered one navigating by GPS only available with active leg at a time CDI Press to change navigation mode on the CDI BACK Press to return to the previous level between GPS NAV and NAV2 softkeys ADF DME optional Press to display the ADF DME IDENT Press to provide special aircraft position Tuning window identification to Air Traffic Control ATC XPDR Press to display the transponder mode selec BACK Press to return to the previous level tion softkeys softkeys STBY Press to select standby mode IDENT Press to provide special aircraft position ON Press to select mode A identification to Air Traffic Control ATC ALT Press to select altitude reporting mode TMR REF Press to display the Timer References VER Press to automatically squawk 1200 only window in the U S A refer to ICAO standards for VFR NRST Press to display the Nearest Airports codes in other countries window ALERTS Press to display the Alerts window rv optional optional optional Ca HA meta ON EN RC ON ND Press the BACK or OFF softkey to return to the top level softkeys Figure 1 3 PFD Softkey Flow Chart 1 Garmin G1000 Cockpit Reference Guide for the DA42 1 5 SECTION 1 SYSTEM OVERVIEW PFD optional Ca RS RC RC RC RC DD Press the DFLTS softkey to change the PFD Press the STD
67. ice alerts are provided to the G1000 are provided to the G1000 by GIA 63 1 Should this unit fail audio and voice alerts will no longer be available system Annunciation Commet Attitude and Heading Reference System is aligning Display system is not receiving attitude information from the AHRS Display system is not receiving airspeed input from air data computer Garmin G1000 Cockpit Reference Guide for the DA42 12 5 SECTION 12 ANNUNCIATIONS amp ALERTS system Annunciation Comment Display is not receiving altitude input trom the air data computer Display is not receiving vertical speed input from the air data computer GPS information is either not present or is invalid for navigation use Note that AHRS utilizes GPS inputs during normal operation AHRS opera tion may be degraded if GPS signals are not present see AFM Display is not receiving valid transponder information _ A red X through any other display field such as engine instrumentation Other Various Red X Indications fields indicates that the field is not receiving valid data 12 6 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 12 ANNUNCIATIONS amp ALERTS A red X may be the result of an LRU or an LRU func tion failure The Figure 12 5 illustrates all possible flags and the responsible LRUs GIA 63 Integrated i z ewe GIA 63 Integrated Avionics Units Avionics Units GDC 74A Air Data Computer en GRS
68. ile and settings lost Recheck settings The pilot may reconfigure the MFD amp PFD with preferred settings if desired XTALK ERROR A flight display The MFD and PFD are not communicating with each other The G1000 system should crosstalk error has occurred be serviced PFD1 SERVICE PFD1 needs service Return unit for repair The PFD and or MFD self test has detected a problem The G1000 system should be MFD1 SERVICE MFD1 needs serviced service Return unit for repair PFD1 CONFIG PFD1 configuration error Contig service req d The PFD and or MFD configuration settings do not match backup configuration MFD1 CONFIG MFD1 configuration memory The G1000 system should be serviced error Contig service req d SW MISMATCH GDU software The MFD and PFD have different software versions installed The G1000 system mismatch Xtalk is off should be serviced MANIFEST PFD1 software mismatch Communication halted The PFD and or MFD has incorrect software installed The G1000 system should be MANIFEST MFD1 software serviced mismatch Communication halted PFD1 COOLING PFD1 has poor cooling Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by dimming MFD1 COOLING MFD1 has poor the display If problem persists the G1000 system should be serviced cooling Reducing power usage PFD1 KEY KEYSTK Key is stuck A key is stuck on the PFD and or MFD bezel Attem
69. ing transmitter power COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM needs service Return unit for repair COM1 PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The GIA1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be serviced The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced The system has detected an over temperature condition in COM1 and or COM2 The transmitter will operate at reduced power If the problem persists the G1000 system should be serviced The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may still be usable The G1000 system should be serviced when possible The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced Garmin G1000 Cockpit Reference Guide for the DA42 12 11 SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63 Message Advisories Co
70. kpit Reference Guide for the DA42 SECTION 12 ANNUNCIATIONS amp ALERTS GDC 74A Message Advisories Alerts Window Message Comments S GDC1 CONFIG GDC1 configuration GDC 74A configuration settings do not match those of backup configuration error Contig service req d memory The G1000 system should be serviced MANIFEST GDC1 software The GDC 74A has incorrect software installed The G1000 system should be mismatch Communication halted serviced BACKUP PATH Airdata using backup The GDC 74A is using a backup communications data path The G1000 system data path should be serviced when possible Miscellaneous Message Advisories Alerts Window Message Comments FPL WPT LOCK Flight plan waypoint Upon power up the G1000 system detects that a stored flight plan waypoint is is locked locked This occurs when an aviation database update eliminates an obsolete way point The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database OR update the waypoint name identitier to reflect the new information FPL WPT MOVE Flight plan The system has detected that a waypoint coordinate has changed due to a new waypoint moved aviation database update Verity that stored flight plans contain correct waypoint locations TIMER EXPIRD Timer has expired T
71. ly set up It is not used during normal operation of the GDL 69 A and it should have no adverse effects if inadvertently selected during flight Refer to the GDL 69 69A XM Satellite Radio Activation Instructions 190 00355 04 Rev E or later for further information Weather Product Age The age for each of the enabled products is displayed on the right side of the display Times are based on Zulu time when the data was assembled on the ground not the time the data was received by the FIS sensor When the age of a weather product has exceeded half of the expiration time the product time will change from light blue to amber in color minutes L SIGMETS AIRMETS fo 60 City Forecasts 60 CountyWarnings 60 CycloneWamnings f 60 FreezingLevels DEAR Surface Analysis o 60 mes Cid 60 WindsAlft 90 ms CT 60 L Cloudstops o Garmin G1000 Cockpit Reference Guide for the DA42 10 4 TRAFFIC INFORMATION SERVICE TIS Displaying Traffic on the Traffic Map Page NOTE If the G1000 is configured to use the optional Skywatch Traffic Advisory System TIS will not be available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site 1 Turn the large FMS knob to select the Map Page Group 2 Turn the small FMS knob to select the Traffic Map Page 3 Press the OPERATE softkey to begin displaying traffic TIS OPERATIING is
72. memory error Contig service req d The G1000 system should be serviced MANIFEST GMA software The audio panel has incorrect software installed The G1000 system should be mismatch Communication halted serviced GMA1 SERVICE GMA1 needs The audio panel self test has detected a problem in the unit Certain audio functions service Return unit for repair may still be available and the audio panel may still be usable The G1000 system should be serviced when possible BACKUP PATH Audio panel using The audio panel is using a backup communication path The G1000 system should backup data path be serviced when possible 12 10 Garmin G1000 Cockpit Reference Guide for the DA42 GIA 63 Message Advisories SECTION 12 ANNUNCIATIONS amp ALERTS Alerts Window Message Comments S GIA1 CONFIG GIA configuration error Contig service req d GIA2 CONFIG GIA2 configuration error Contig service req d GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair MANIFEST GIA1 software mismatch Communication halted MANIFEST GIA2 software mismatch Communication halted COM1 TEMP COMT over temp Reducing transmitter power COM2 TEMP COM over temp Reduc
73. mercial distribution of this manual or any revision hereto is strictly prohibited Garmin is a registered trademark of Garmin Ltd or its subsidiaries and G1000 is a trademark of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin NavData is a registered trademark of Jeppesen Inc Stormscope is a registered trademark of L 3 Communications November 2005 190 00406 03 Rev B Printed in the U S A Garmin G1000 Cockpit Reference Guide for the DA42 WARNINGS CAUTIONS amp NOTES WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain function The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated
74. nces window Press the TMR REF softkey to display the widow When active ON the Vspeeds are displayed at their respective locations to the right of the airspeed scale To activate the Vspeed References dis play the Timer Reference window and turn the large FMS knob to place the cursor in the ON OFF field Turn the small FMS knob to select ON or OFF 2 2 ATTITUDE INDICATOR The Slip Skid Indicator is located under the roll point er and moves laterally away from the pointer to indicate lateral acceleration One Slip Skid indicator displacement is equal to one ball displacement when compared to a tra ditional slip skid indicator AO Roll Pointer Roll Scale 6 Aircraft Wing Tips E Pitch Scale 3 Horizon Line Slip Skid Indicator Aircraft Symbol 0 Sky Representation 5 Land Representation Roll Index Figure 2 6 Attitude Indicator Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 2 FLIGHT INSTRUMENTS 2 3 ALTIMETER Altitude Reference Box Altitude Trend Current Altitude Vector Altitude Reference Bug EE E Barometric Setting Box Figure 2 7 Altimeter Altitude Reference Bug The Altitude Reference Bug can be set to any desired altitude The bug acts as a visual reference to indicate the desired altitude is approaching To set the altitude reference bug 1 Turn the ALT knobs to set the altitude reference bug The small ALT knob sets the hundreds and the large ALT k
75. ndicator 2 4 2 5 Marker Beacon Annunciations 0 2 2 6 Vertical Speed Indicator 0 ccs 2 5 2 7 Horizontal Situation Indicator HSI 2 5 CUES POINT a enhance stasis 2 6 Course Deviation Indicator CDI 2 6 Bearing Pointers and Information Windows 2 6 DME Radio optional ner 2 7 Navigation S OUNCE sas deinen amet 2 7 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 1 3 1 Engine Display 3 1 3 2 FUEL Display 00 0 0 cece eesteeseesean 3 1 3 3 Engine System Display 3 2 SECTION 4 NAV COM AND TRANSPONDER 4 1 4 1 Radio Status Indications 4 3 4 2 Volume 4 3 4 3 Automatic Squelch 4 3 4 4 Quickly Activating 121 500 MHz 4 3 4 5 Optional NAV Radios 0 0 ccseeeen 4 3 ADF Radio optional 4 3 DIVE RAI lOD ICRA 4 4 4 6 Frequency Auto tuning 0 cccsseseen 4 4 Auto tuning on the PFD cscessesscestesssestesseesesseeseeaees 4 4 Auto tuning on the MFD sssri 4 4 TABLE OF CONTENTS 4 1 Transponder 4 5 Mod Selection 4 5 Ground Mode Automatic 4 5 ROD IV STATUS iaasa a ase rE OENES 4 5 RE TEE N AEE A 4 5 Fiant ID REDON mnt 4 5 SECTION 5 AUDIO PANEL 5 1 5 1 COM Radio Selection 5 2 5 2 Marker Beacon Receiver 5 2 Marker Beacon Signal Sensitivity c ssesesesseesneessen 5 2 5 3 Navigation Radio
76. next transmission is received it is recorded in the next memory block and so on Once the 2 5 minutes of recording time has been reached the recorder begins recording over the stored memory blocks starting from the oldest block Powering off the unit automatically clears all recorded blocks v v MAN SQ PLAY Figure 5 8 Playback e Pressing PLAY once plays back the latest recorded memory block then returns to normal operation Pressing PLAY during playback of a memory block halts the playback of this block and plays back the preceding recorded block The PLAY key can be used to backtrack through the recorded memory blocks to reach and play back any desired block Pressing the MKR MUTE key during playback halts playback and returns the recorder playback to normal operation If a COM input signal is detected during playback playback is halted and the new COM input signal is re corded as the latest block 5 4 Garmin G1000 Cockpit Reference Guide for the DA42 FLIGHT CONTROL SECTION 6 AUTOMATIC FLIGHT CONTROL Refer to the pilots guide for the installed autopilot sys tem Garmin G1000 Cockpit Reference Guide for the DA42 6 1 SECTION 6 AUTOMATIC FLIGHT CONTROL This page intentionally left blank 6 2 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 7 NAVIGATION The following discussions pertain to the Multi function Display unless otherwise indicated 7 1 NAVIGATION MAP PAGE Select t
77. ning for totalizer calculations A NOTE Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 3 ENGINE SYSTEM DISPLAY Engine Load Indicator Voltmeter Gearbox Temperature Indicator Oil Temperature _ Indicator Deice Fluid J Indicator Tachometer RPH ELECTRICAL 25 VOLTS 25 4 4 O Ans O g Ammeter g To ENGINE _ GEARBOK 3 TC a COOLANT Coolant a BO S Temperature OTL Indicator 50 OSD 23 BAR 23 Oil Pressure Indicator DEICE FLUID N A Figure 3 3 DA42 SYSTEM Page 3 2 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 4 NAV COM amp TRANSPONDER SECTION 4 NAV COM AND TRANSPONDER The Nav Com controls and frequency windows are lo cated on the Primary Flight Display and the Multi Func tion Display in the same locations NAV COM Controls NAV Frequency Window COM Frequency Window Controls navi 13 25 110 90 er ESTI ns 199 95 mk 095 f 118 900 133 800 com 110 90 238 135 325 cz 1000 CRS 4 BARO PUSH CAS CTA 650A RANGE ER iki 15TH Ar POE INSET FD CD OBS XPDR IDENT TMR REF Figure 4 1 G1000 VHF NAV COM Interface PFD Garmin G1000 Cockpit Reference Guide for the DA42 4 1 SECTION 4 NAV COM amp
78. nob sets the thousands This altitude also appears in the altitude reference box above the altimeter Altitude Trend Vector The end of the trend vector displays approximately what the altitude will be in 6 seconds if the current rate of vertical speed is maintained Barometric Setting Box To set barometric pressure turn the BARO knob to select the desired setting 2 4 VERTICAL DEVIATION GLIDESLOPE INDICATOR The Vertical Deviation Glideslope Indicator appears when an ILS is tuned in the active NAV field 2 5 MARKER BEACON ANNUNCIATIONS Marker Beacon Annunciation Vertical Deviation Glideslope Indicator Figure 2 8 Marker Beacon and Vertical Deviation Garmin G1000 Cockpit Reference Guide for the DA42 2 6 VERTICAL SPEED INDICATOR Vertical Speed Pointer Figure 2 9 Vertical Speed Indicator The actual vertical speed is displayed inside the point er 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 SECTION 2 FLIGHT INSTRUMENTS A Turn Rate Indicator 2 Lateral Deviation Scale G Navigation Source Aircraft Symbol 5 Course Deviation Indicator 6 Rotating Compass Rose 7 OBS Mode TO FROM Indicator C Heading Bug 10 Course Pointer Flight Phase Turn Rate and Heading Trend Vector 13 Heading Lubber Line Figure 2 10 Horizontal Situa
79. nt Alerts Window Message COM1 RMT XFR COM1 remote transfer key is stuck COM2 RMT XFR COM remote transter key is stuck RAIM UNAVAIL RAIM is not available trom FAF to MAP waypoints RAIM UNAVAIL RAIM is not available POSN ERROR RAIM has determined GPS position is in error DGRD GPS ACC GPS position accuracy degraded amp RAIM unavailable GPS1 FAIL GPS1 is inoperative GPS2 FAIL GPS is inoperative GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair NAV1 RMTXFR NAV1 remote transfer key is stuck NAV2 RMTXFR NAV2 remote transfer key is stuck The COM1 and or COM transfer switch is stuck in the enabled or pressed posi tion Press the transter switch again to cycle its operation If the problem persists the G1000 system should be serviced GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity Monitoring RAIM trom the FAF to the MAP waypoints GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity Monitoring RAIM for the current phase of flight When a RAIM position error is detected GPS is tlagged and the system no longer provides GPS based guidance GPS position accuracy has been degraded and RAIM is not available A failure has
80. og storage location 4 With OK highlighted press the ENT key to invert the flight plan PAGE MENU OPTIONS Store Flight Plon Twert Flight Plon OO Delete Flight Plan Press the FMS CRSR knob to return to bose poge Figure 8 15 Invert Flight Plan 8 16 COPY A FLIGHT PLAN 1 From the Flight Plan Catalog press the FMS knob to activate the cursor turn the large FMS knob to highlight the flight plan to be copied then press the MENU key to display the Flight Plan Catalog Options 2 Turn the large FMS knob to highlight Copy Flight Plan and press the ENT key 3 A Copy to flight plan confirmation window is displayed With OK highlighted press the ENT key to copy the flight plan To cancel turn the large FMS knob to highlight CANCEL and press the ENT key 8 17 DELETE A FLIGHT PLAN 1 From the Flight Plan Catalog Page press the FMS knob to activate the cursor turn the large FMS knob to highlight the flight plan to be deleted 8 18 8 19 Press the MENU key to display the Flight Plan Catalog options Turn the large FMS knob to highlight Delete Flight Plan and press the ENT key A Delete flight plan confirmation window is displayed With OK highlighted press the ENT key to delete the flight plan To cancel turn the large FMS knob to highlight CANCEL and press the ENT key GRAPHICAL FLIGHT PLAN CREATION Press the FPL key to display the Active Flight Plan Page
81. on loading and activating departure procedures 8 9 LOAD AN ARRIVAL See the Procedures section for a discussion on loading and activating arrival procedures 8 10 LOAD AN APPROACH See the Procedures section for a discussion on loading and activating approach procedures Garmin G1000 Cockpit Reference Guide for the DA42 8 11 REMOVE A DEPARTURE ARRIVAL OR APPROACH FROM A FLIGHT PLAN 1 With the Active or Stored Flight Plan Page dis played press the small FMS knob to activate the cursor 2 Turn the large FMS knob to highlight the title for the approach departure or arrival to be deleted Titles appear in white directly above the procedure s waypoints 3 Press the CLR key to display a confirmation window With OK highlighted press the ENT key to remove the selected procedure 8 12 STORE A FLIGHT PLAN 1 From the Flight Plan Page press the FMS knob to activate the cursor 2 Turn the large FMS knob to highlight the desired flight plan and press the MENU key to display the Flight Plan Page options 3 Turn the large FMS knob to highlight Store Flight Plan and press the ENT key 4 With OK highlighted press the ENT key to store the flight plan Figure 8 13 Store Flight Plan Confirmation EDIT A STORED FLIGHT PLAN 1 Press the FPL key and turn the small FMS knob to display the Flight Plan Catalog Page 2 Press the FMS knob to activate the cursor 3 Turn the large FMS knob to highlight th
82. ow Text Alerts Window Message Audio Alert L R GLOW ON Left right engine glow plug active No Tone L R FUEL XFER Left right fuel transfer from aux to main in progress Message Advisory Alerts Alerts Window Message Audio Alert PFD FAN FAIL The cooling fan for the PFD is inoperative MFD FAN FAIL The cooling fan for the MFD is inoperative GIA FAN FAIL The cooling fan for the GIAs is inoperative 12 4 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 12 ANNUNCIATIONS amp ALERTS 12 3 G1000 SYSTEM ANNUNCIATIONS Traffic Voice Alerts When an LRU or an LRU function fails a large red The following voice alerts can be configured for Male X is typically displayed on windows associated with the Of Female gender by using the Aux System Setup Page failed data The following section describes various sys OR the MFD tem annunciations Refer to the Aircraft Flight Manual for additional information regarding pilot responses to these Sava Aert on TA i ralnic ayed wnen a Ifalllc AQVISOry Issued A NOTE Upon power up of the G1000 system Traffic Not certain windows remain invalid as G1000 equip Available cannot communicate ment begins to initialize All windows should be operational within one minute of power up Should any window continue to remain flagged A the G1000 system should be serviced by a Garmin authorized repair facility annunciations NOTE Voice NOTE Vo
83. pt to free the stuck key by press MFD1 KEY KEYSTK Key is stuck ing it several times The G1000 system should be serviced if the problem persists CNFG MODULE PFD1 configuration The PFD configuration module backup memory has failed The G1000 system should module is inoperative be serviced 12 8 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 12 ANNUNCIATIONS amp ALERTS Database Message Advisories Alerts Window Message Comments o MFD1 DB ERR MFD1 aviation database error exists The MFD and or PFD detected a failure in the aviation database Attempt to reload PFD1 DB ERR PFD aviation the aviation database It problem persists the G1000 system should be serviced database error exists MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database The MFD and or PFD detected a failure in the basemap database The MFD and or PFD detected a failure in the terrain database Ensure that the ter rain card is properly inserted in display Replace terrain card If problem persists The G1000 system should be serviced error exists DB MISMATCH Aviation database The PFD and MFD have different aviation database versions installed Crossfill is off version mismatch Xtalk is off Install correct aviation database version in both displays DB MISMATCH Aviation
84. r TIS ser vice becomes unavailable Garmin G1000 Cockpit Reference Guide for the DA42 10 7 SECTION 10 HAZARD AVOIDANCE 10 5 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 the Terrain Proximity Page 1 Turn the large FMS knob to select the Map Page Group 2 Turn the small FMS knob to select the last rectangular page icon 3 If desired press the VIEW softkey to access the ARC and 360 softkeys When the ARC softkey is pressed a radar like 120 view is displayed Press the 360 softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 136 975 Figure 10 12 Terrain Proximity Page WARNING Terrain Obstacle at or within 100 below current aircraft altitude CAUTION Terrain Obstacle between 100 and 1000 below current aircraft altitude roe Aircraft Altitude 1 400 Threshold Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed press the MAP softkey 2 Press the TERRAIN softkey Terrain and obstacle proximity will now be displayed on the map Maximum ELEV FT oa of MAX 1 6 F topo o presently MIN 577 Isp Rae on screen Im I Minimum or of topograph fi presently isplayed on screen
85. rmation on the G1000 MFD is approved for weather avoidance only Refer to the WX 500 Pilot s Guide for detailed opera tion Displaying Stormscope Lightning Data on the Navigation Map Page 1 Press the MAP softkey 2 Press the STRMSCP softkey Press the STRMSCP softkey again to remove Stormscope Lightning Data from the Navigation Map Page J NEXRAD YH LTNG Figure 10 4 In Flight Navigation Map Page Displaying Stormscope Lightning Data Lightning Age symbol Strike is less than 6 seconds old Strike is between 6 and 60 seconds old Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Garmin G1000 Cockpit Reference Guide for the DA42 10 1 SECTION 10 HAZARD AVOIDANCE At a map range of less than 25 nm Stormscope light ning data is not displayed but can still be present The presence of Stormscope lightning data is indicated by the annunciation LTNG lt 25 nw in the upper right corner NORTH UP LTNING MODE CELL oe 1 a N Fe PET LL a we LL J b iat i l Figure 10 5 Lightning Display Range Annunciation To select cell or strike as the Stormscope lightning mode 1 With the Weather Group selected press the ENT key The cursor flashes on STRMSCP LING Turn the large FMS knob to select STRMSCP MODE Turn either FMS knob to display the Cell Strike window Turn either FMS knob to select Cell or Strike Press the ENT key
86. ser 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 aircraft position 2 After placing the pointer at the desired posi tion press the ENT key The User Waypoint Information Page is now displayed with the captured position 3 Turn the FMS knobs to select a waypoint name 4 Press the ENT key to accept the selected name The first reference waypoint field is highlighted 5 If desired turn the FMS knobs to enter the identifier of the reference waypoint and the radial and distance to the reference waypoint Press the ENT key to accept 6 Press the FMS knob to remove the flashing Cursor Garmin G1000 Cockpit Reference Guide for the DA42 8 1 SECTION 8 FLIGHT PLANNING Modify a User Waypoint 1 With the User Waypoint Information Page j displayed press the FMS knob to activate the AR sep ete cursor MOODS inf 127 2 Turnthe large FMS knob to move the cursor to Figure 8 3 Active Flight Plan Window on the PFD the desired field and turn the small FMS knob RME 8 3 ACTIVATE A STORED FLIGHT PLAN 3 Press the ENT key to accept the changes 4 Press the FMS knob to remove the flashing l Press the FPL key and turn the small FMS knob de to display the Flight Plan Catalog Page Delete a User Waypoint 1 Select the User Waypoint Information Page and press MENU to display the User Waypoint
87. st Intersections 0 c ccc 1 6 Select the Nearest Intersections Page 7 6 View Information on the Nearest Intersection 7 7 7 10 Nearest NDB 000 scenes 1 1 Select the Nearest NDB Page 7 7 Access Information on a Specific NDB 7 1 7 11 Nearest VOR sce ot 1 1 Select the Nearest VOR Page c ssessesesseesseeseeresseean 7 7 View Information on the Nearest VOR 7 7 Select and Load a VOR Frequency 1 8 7 12 Nearest User Waypoint 1 8 Select the Nearest User Waypoint Page 1 8 Select a Nearest User Waypoint c sceseseesecsesseaseean 1 8 7 13 Nearest Frequencies 0 cccccccesseseseeseenees 1 8 Select the Nearest Frequencies Page 1 8 Select and Load the Nearest ARTCC FSS or Weather PEE E NICU ARS AN ores 1 9 7 14 Nearest Airspaces 7 9 Select the Nearest Airspaces Page 7 9 AISDaCOAIGITS BOX cas 2c ascsssacosateamanccenverasnmenccawarnss 7 9 View Additional Details for a Listed Airspace 7 9 View and Quickly Load the Frequency for a Controlling AOON sacattnasncdetineu a EED LS SECTION 8 FLIGHT PLANNING 8 1 8 1 User Defined Waypoints 8 1 Select the User WPT Information Page scssesseseeen 8 1 Create a New User Waypoint 8 1 Create User Waypoints from the Navigation Map Page 8 1 Modify a User Waypoint scssessssessessessneesnessen 8 2 Delete a Us
88. tem should be serviced MANIFEST GEA1 software mismatch Communication halted BACKUP PATH EIS using backup The GEA 71 is using a backup communication path The G1000 system should be data path serviced when possible GTX 33 Message Advisories Alerts Window Message Comments o XPDR1 CONFIG XPDR1 contig error The transponder configuration settings do not match those of backup configuration Contig service req d memory The G1000 system should be serviced The GEA 71 has incorrect sottware installed The G1000 system should be serviced MANIFEST GTX1 software mismatch The transponder has incorrect software installed The G1000 system should be Communication halted serviced BACKUP PATH Transponder using The transponder is using a backup communications path The G1000 system should backup data path be serviced when possible Garmin G1000 Cockpit Reference Guide for the DA42 12 13 SECTION 12 ANNUNCIATIONS amp ALERTS GRS 77 Message Advisories Alerts Window Message Comments S AHRS TAS AHRS not receiving The AHRS is not receiving true airspeed from the air data computer The AHRS relies airspeed on GPS information to augment the lack of airspeed The G1000 system should be serviced AHRS GPS AHRS using backup GPS The AHRS is using the backup GPS path Primary GPS path has failed The G1000 source system should be serviced when possible AHRS GPS AHRS not receiving GPS
89. th the compass lubber line 5 Joystick Changes the map range when rotated Ac tivates the map pointer when pressed 6 CRS BARO Knob The large knob sets the altim eter barometric pressure and the small knob adjusts the course The course is only adjustable when the HSI is in VORI VOR2 or OBS SUSP mode Pressing this knob centers the CDI on the currently selected VOR 7 Dual COM Knob Tunes the MHz large knob and kHz small knob standby frequencies for the COM trans ceiver Pressing this knob toggles the tuning cursor light blue box between the COMI and COM2 fields 8 COM Frequency Toggle Key Toggles the standby and active COM frequencies Pressing and holding this key for two seconds automatically tunes the emergency frequency 121 5 MHz in the active frequency field 9 COM VOL SQ Knob Controls COM audio level Pressing this knob turns the COM automatic squelch ON and OFF Audio volume level is shown in the field as a percentage 10 Direct to Key Allows the user to enter a destina tion waypoint and establish a direct course to the selected destination specified by the identifier chosen from the active route or taken from the map cursor position 11 FPL Key Displays the active Flight Plan Page for creating and editing the active flight plan or for accessing stored flight plans SECTION 1 SYSTEM OVERVIEW 12 CLR Key DFLT MAP Erases information can cels an entry or removes page menus
90. tion Indicator Garmin G1000 Cockpit Reference Guide for the DA42 2 5 SECTION 2 FLIGHT INSTRUMENTS Turn Rate Indicator and Heading Trend Vector Each tick mark is at 9 half standard rate tick mark and 18 standard rate tick mark degrees to the left and right of the lubber line A wide magenta line displays the current turn rate up to 24 degrees A magenta arrow head appears at 25 degrees This trend vector provides the pilot with a prediction of what the heading will be in 6 seconds at the present turn rate A Figure 2 14 Turn Rate Indicator and Heading Trend Vector Course Pointer The course pointer is a single line arrow GPS VORI and LOC1 or double line arrow VOR2 and LOC2 which points in the direction of the set course Course Deviation Scale TO FROM Indicator Lateral Deviation Figure 2 15 Arc CDI and Compass Rose CDI Course Deviation Indicator CDI The CDI scale automatically adjusts to the current phase of flight enroute 5 0 nm terminal area 1 0 nm or approach 0 3 nm Scaling may be selected manually from the MFD System Setup Page See the MFD Pilots Guide for more detail 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 pointer un Information Bearing 1 Window Pointer Bearing 2 Pointer Bearing 1 Bearing 2 Information Inform
91. up of softkeys for additional weather control SFC pressing the SFC softkey for Surface Analysis shows current or forecast conditions Forecasts are available for intervals of Current 12 24 36 and 48 hours Press the softkey corresponding to the desired forecast The closest city forecast information is displayed in the legend The dis play is updated every 12 minutes FRZ LVL press the FRZ LVL softkey to display contour lines for freezing levels The display is updated every 12 minutes WIND press the WIND softkey to show wind speed and direction at a selected altitude from the ground up to 42 000 feet in 3 000 foot incre ments After pressing the WIND softkey press the softkey corresponding to the desired winds aloft altitude The display is updated every 12 minutes COUNTY pressing the COUNTY softkey provides specific public awareness and protection weather warnings for Tornado Severe Thunderstorm and Flood conditions provided by the National Weather Service NWS The display is updated every 5 minutes SECTION 10 HAZARD AVOIDANCE CYCLONE pressing the CYCLONE softkey shows the current location of cyclones hurricanes and tropical storms and their projected track at vari ous time intervals The update rate is every 12 minutes Map Panning Information Weather Data Link Page 1 Push in the joystick to display the panning arrow 2 Move the joystick to place the panning arrow onAIRMETs TFRs META
92. vided by the GDL 69 is approved only for weather avoidance not penetration Garmin G1000 Cockpit Reference Guide for the DA42 W 1 WARNINGS CAUTIONS amp NOTES WARNING NEXRAD weather data is to be used for long range planning purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD weather data should not be used for short range weather avoidance WARNING The Garmin G1000 as installed in the Diamond DA42 aircraft has a very high degree of func tional integrity However the pilot must recognize that providing monitoring and or self test capability for all conceivable system failures is not practical Although unlikely it may be possible for erroneous operation to occur without a fault indication shown by the G1000 It is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVI gation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or
93. window is displayed by pressing the ADF Auto tuning on the PFD DME softkey if no ADF is installed the softkey will be labeled DME NEAREST AIRPORTS 124 6 8NM VFR 122 704 RNWY 2440FT 270 10 2NM ILS 123 000 RNWY 57 FT ADF DME TUNING ADF 198 0 MODE4BFO vo 507 DME MODE WEVA 150 11 4NH ILS 133 006 RNWY 7339FT LCL por 2345 ON LCL 013818 IDENT THR REF RES CAUTION Figure 4 8 Radio Tuning Window Figure 4 10 Nearest Airports Window PFD To change the DME tuning source 1 Press the NRST softkey to display the Nearest 1 From the Tuning window turn the large FMS Airports Window knob to highlight the DME source field 2 Turn the FMS knobs to highlight the desired f 2 Turn the small FMS knob to display the selec DE tion window Turn the FMS knobs to select the desired mode and press the ENT key 3 Press the ENT key to place the frequency in the standby field of the active COM 4 Press the Frequency Toggle key to place the frequency in the active field NAV frequencies are entered automatically in the NAV window upon approach loading or approach activation Figure 4 9 DME Selection Window Auto tuning on the MFD Auto tuning on the MFD is done in much the same way as on the PFD Use the FMS knobs to select the de sired frequency on any of the information pages Pressing the ENT key then loads the selected frequency into the standby frequency window of the appropriate radio
94. y to show the location elevation and direction the high est radar echo This may not indicate the top of a storm or clouds only the highest radar return echo ECHO TOPS cannot be displayed along with NEXRAD and CLOUD TOPS When ECHO TOPS is activated NEXRAD and CLOUD TOPS are removed Refer to the Legend for a descrip tion of the ECHO TOPS coding The display is updated every 7 5 minutes CLD TOP press the CLD TOP softkey to show the cloud top altitude determined from satellite imagery The display is updated every 15 minutes LING pressing the LING softkey shows the location of cloud to ground lightning strikes The display is updated every five minutes NOTE Strikes depicted represent cloud to ground strikes within a 2 kilometer radius of the actual strike location Therefore the exact location of the strike is not displayed Garmin G1000 Cockpit Reference Guide for the DA42 CELL MOV pressing the CELL MOV softkey shows storm cell movement by displaying an arrow point ing in the direction of predicted movement The display is updated every 12 minutes SIG AIR pressing the SIG AIR softkey shows SIGMET and AIRMET information The display is updated every 12 minutes METAR press the METAR softkey to graphically dis play METARs METARS are shown as colored flags at airports providing METAR reports The display is updated every 12 minutes MORE WX press the MORE WX softkey to display the following gro

Garmin Software Version 0370.13 Cockpit Reference Guide

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