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Garmin Software Version 0370.14 Cockpit Reference Guide

1. 1 5 Access Runway Information for the Selected ANDON ne nn tes 1 6 Quickly Tune the COM Transceiver to a Nearby ANOO Frogu sonia anni 1 6 Nearest Airports Information on the PFD 7 6 View Information on a Specific Airport in the List 7 6 Load an Airport COM Frequency into the AEC ON os sae none nee ons 1 6 7 9 Nearest Intersections 0 ccc l 1 Select the Nearest Intersections Page 7 7 View Information on the Nearest Intersection 7 1 7 10 Nearest NDB 000 cscs 1 1 Select the Nearest NDB Page 7 7 Access Information on a Specific NDB l 1 7 11 Nearest VOR ssh 1 8 Select the Nearest VOR Page c sssessessessseseesessessean 1 8 View Information on the Nearest VOR 1 8 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 ssessessessesesseeee 1 8 7 13 Nearest Frequencies 0 c ccccceseseseeseeeees 1 9 Select the Nearest Frequencies Page 7 9 Select and Load the Nearest ARTCC FSS or Weather Frequency 7 9 7 14 Nearest Airspaces 7 9 Select the Nearest Airspaces Page 7 9 Airspace Alerts BOX corineus 7 9 View Additional Details for a Listed Airspace 7 10 View and Quickly Load the Frequency for a COMMING AGENCY earth 7 10 SECTION 8 FLIGHT PLANNING 8 1 8 1 User Defined Waypoints
2. 8 1 Select the User WPT Information Page scsesseseeen 8 1 Create a New User Waypoint 8 1 Modify a User Waypoint sssssssssssssssssssssssssrrrrnerenn 8 1 Delete a User Waypoint seessesssssessesessesseesessen 8 1 Create User Waypoints from the Navigation Map Page 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 8 3 8 5 Stop Navigating a Flight Plan 8 3 8 6 Invert Active Flight Plan 8 3 8 1 Create a New Flight Plan 8 4 Create a New Flight Plan Using the MFD uv 8 4 Create a New Flight Plan Using the PFD nsss 8 4 8 8 Load a Departure oo ccs 8 5 8 9 Load an Arrival 8 5 8 10 Load an Approach 8 5 8 11 Remove a Departure Arrival or Approach from a Flight Plan 8 5 8 12 Store a Newly Created 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 6 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 8 20 Vertical Navigation VNAV Page 8 8 Create a Vertical Navigation Profile 8 8 VNAV Page Ment OPTIONS stats 8 9 SECTION 9 PROCEDURES 00 0 0 9 1 9 1 Arrivals and Departures 9 1 Load and Activate a Departure Procedure
3. 11111 9 1 Load and Activate An Arrival Procedure 9 1 9 2 Approaches 55 8 nt 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 11111seeeeen 10 1 Displaying Stormscope Lightning Data on the Navigation MAD PAR 10 1 LOSCO DEF Eceran 10 2 ii Garmin G1000 Cockpit Reference Guide for the DA42 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 NEXRADNAIOTIONS TES ne 10 4 Map Panning Information Weather Data Link Page 10 5 Weather Products and Symbols csseseseseeseesen 10 6 Weather Product Age csssessssssssssessesssesneeseessen 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 8 TSI MENT enter ananas 10 8 10 5 Traffic Advisory System TAS Optional 10 8 Honeywell KTA 870 10 8 SEM SEM TOS rate 10 8 Displaying Traffic on the Traffic Map Page 10 8 Displaying Traffic on the Navigation Map 10 9 Avidyne TAS600 Series 10 9 Displaying Traffic on the Traffic Map Page 10 9 Displaying Traffic on the Navigation Map 10
4. FLIGHT ID Flight ID Figure 4 13 Timer References Window Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 4 NAV COM amp TRANSPONDER Blank Page 4 6 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 5 AUDIO PANEL SECTION 5 AUDIO PANEL COMI com i Transmitters _ nd me Transceiver Audio COM3 MIC is unavailable MIC COM2 COM 3 is unavailable COM3 Split COM Not recommended on the Telephone Unavailable Passenger Address Speaker Marker Beacon Mute Marker Beacon Signal Sensitivity Es Aircraft Navigation Radio Audio Aircraft Navigation Radio Audio ADF amp DME optional AUX unavailable Manual Squelch RSS Recorded COM Audio Playback chew ac SORA ICS Isolation ICS ISOLATION PILOT O 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 Jz 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 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
5. CAUTIONS amp NOTES CAUTION The Garmin G1000 does not contain any user serviceable parts Repairs should only be made 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 RECORD OF REVISIONS Part Number Change Summary 190 00406 01 Added DME capability Added BRG1 BRG2 pointers Changed Airspeed Trend Vector Changed Altitude Trend Vector Added Checklist capability Adde
6. From the tuning window turn the large FMS Knob to highlight the DME source field 2 Turn the small FMS Knob to display the selection window Turn the FMS Knobs to select the desired mode and press the ENT Key FREQUENCY AUTO TUNING Auto tuning on the PFD NEAREST AIRPORTS 124 6 8NM VFR 122 700 RNHY 2440FT 210 10 2N ILS 123 000 RNWY 57 0 FT 150 11 4NM ILS 133 000 RNWY 7339FT LCL por 2345 ON LCL 013818 IDENT THR REF NRST CAUTION Figure 4 10 Nearest Airports Window PFD Press the NRST Softkey to display the Nearest Airports Window Turn the FMS Knobs to highlight the desired frequency Press the ENT Key to place the frequency in the standby field of the active COM Press the Frequency Toggle Key to place the frequency in the active field NAV frequencies are entered automatically in the NAV active frequency field 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 desired frequency on any of the information pages Pressing the ENT Key then loads the selected frequency in the tuning box as a standby frequency 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 air
7. SECTION 1 SYSTEM OVERVIEW This guide gives the pilot abbreviated operating instructions 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 operating System instructions on the major features of the G1000 system ee more easily It is not intended to be a comprehensive A NOTE The pilot should read and thoroughly operating guide Complete operating procedures for the understand the Aircraft Flight Manual AFM complete system are found in the G1000 Diamond DA42 y AOR p coe ae KA Elanora Pilots Guide 190 00649 00 information not contained in this Cockpit Reference Guide The Aircraft Flight Manual always takes precedence over the information found in this guide 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 T
8. G1000 Cockpit Reference Guide for the Diamond DA42 Copyright 2004 2006 Garmin Ltd or its subsidiaries All rights reserved This manual retlects the operation of System Software version 0370 14 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 comm
9. System Annunciation Comment Attitude and Heading Reterence System is aligning Display system is not receiving attitude information from the AHRS Display system is not receiving airspeed input trom air data computer Display is not receiving altitude input trom the air data computer Garmin G1000 Cockpit Reference Guide for the DA42 12 5 SECTION 12 ANNUNCIATIONS amp ALERTS system Annunciation Comment SS Display is not receiving vertical speed input trom the air data computer GPS information is either not present or is invalid tor 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 function failure The Figure 12 5 illustrates all possible flags and the responsible LRUs GIA 63 Integrated Avionics Units a a U GEA 71 Engine FUEL FLOW Airframe Unit pii GIA 63 Integrated neiaa Avionics Unit ECU OIL PRES COOLANT TEHP FUEL TEMP ICh FUEL QTY GAL oe lt lt 10 15 Z0 Zb ENGINE PFD 08S CDI ADF DME G
10. 2 Press the small FMS Knob to activate the cursor PFD DSPL gt AUTO is now highlighted 3 Turn the small FMS Knob to display the selection window Figure 1 8 PFD Setup Menu 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 highlight 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 25 110 90 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 Box 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 Box 7 System Time Box 15 Navigation Status Box Transponder Status Box Slip Skid Indicator 17 Attitude Indicator Figure 2 1 Default PFD Information Garmin G1000 Cockpit Reference Guide for the
11. 4000 Figure 2 8 Altitude Alerting Visual Annunciations Altitude Trend _ Current Altitude Visual annunciations appear in the Altitude Reference va Box Whenever the Altitude Reference is changed the Altitude Alerter is reset The Altitude Alerter is independent of the Automatic Flight Control System Altitude Reference Bug 30 050 Barometric Setting Box 2 4 VERTICAL DEVIATION GLIDESLOPE INDICATOR The Vertical Deviation Glideslope Indicator appears The Altitude Reference Bug can be set to any desired when an ILS is tuned in the active NAV frequency field altitude The bug acts as a visual reference to indicate the desired altitude is approaching 2 5 MARKER BEACON ANNUNCIATIONS To set the altitude reference bug Figure 2 7 Altimeter Altitude Reference Bug Turn the ALT Knobs to set the altitude reference eee bug The small ALT Knob sets the hundreds and the large ALT Knob sets the thousands This altitude also appears in the Altitude Reference Box above the altimeter ca _ Vertical Altitude Trend Vector ae 7 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 Figure 2 9 Marker Beacon and Vertical Deviation To set barometric pressure turn the BARO Knob to select the desired setting 2 4 Garmin G1000 Cockpit Reference Guide for the DA42 2 6 VERTICAL SPEED INDICATOR Vertical Speed Poin
12. e An individual NEXRAD site cannot depict high altitude storms at close ranges and has no 3 Press the available softkeys to select the desired XM weather product 4 Press the LEGEND Softkey to view the legends information about storms directly over the site for the selected products If necessary turn The resolution of displayed NEXRAD data is 2 either FMS Knob to scroll through the list kilometers Therefore when zoomed in on the Press the small FMS Knob or the ENT Softkey display each square block is 2 kilometers on each to return to the map side The intensity level reflected by the square will be the highest level sampled within the square area 10 4 Garmin G1000 Cockpit Reference Guide for the DA42 ECHO TOP Press the ECHO TOP Softkey to show the location elevation and direction the highest radar echo This may not indicate the top of a storm or clouds only the highest radar return echo 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 description 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 depict
13. edited This alert is issued only after an aviation database update Verify 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 roi Lin te Aircraft is approaching target altitude Prepare to level aircratt 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 from flight plan Update flight plan with current waypoint muha Arriving at waypoint xxxx where xxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft 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 Garmin G1000 Cockpit Reference Guide for the DA42 12 15 SEC
14. 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 The AHRS has incorrect software installed The G1000 system should be serviced Garmin G1000 Cockpit Reference Guide for the DA42 12 13 SECTION 12 ANNUNCIATIONS amp ALERTS GMU 44 Alert Messages Alerts Window Message Comments HDG FAULT 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 GDL 69 Alert Messages Alerts Window Message Comments S O GDL69 CONFIG GDL 69 configura GDL 69 configuration settings do not match those of backup configuration memory tion error Config service req d The G1000 system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced The GMU 44 has incorrect software installed The G1000 system should be serviced GDC 74A Alert Messages Alerts Window Message Comments S O GDC1 CONFIG GDC1 configuration GDC 74A configuration settings do not match those of backup configuration error Config service req d memory The G1000 system should be serviced MANIFEST GDC1 software The GDC 74A has incorre
15. 1 2 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 closest 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 Figure 7 8 VOR Information Page Select the VOR Information Page 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the fourth rectangular page icon Access Information on a VOR 1 With the VOR Information Page displayed press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to highlight the desired selection field identifier name or closest city 3 Turn the FMS Knobs to enter an identifier name or city and press the ENT Key 4 The FREQUENCY field is now highlighted If desired press the ENT Key to place the frequency in the NAV receiver standby frequency field 5 Press the FMS Knob to remove the cursor SECTION 7 NAVIGATION 7 7 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user defined waypoints 7 8 NEAREST AIRPORTS 1795 f BEGRIE NEAREST AIRPORTS day Fi D z INFORMATION rs i T i a A Figure 7 9 Nearest Airports Page Nearest Airport I
16. 10 10 6 Terrain And Obstacle Proximity 10 10 Displaying Terrain and Obstacles on the Terrain POX PAG a dde 10 10 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 11 4 Stormscope Operation with Loss of Heading Input 11 2 SECTION 12 ANNUNCIATIONS amp ALERTS 12 1 12 1 Alert Level Definitions 0 0 cccee 12 2 12 2 Aircraft Alerts 12 3 WARNING ABS sereine 12 3 CAUTION ACHES nement 12 3 Annunciation Advisory Alerts 12 4 Message Advisory Alerts 12 4 TIS Voice Ales ni ae 12 4 12 3 G1000 System Annunciations 12 5 Mn es Sa en ie theta 12 5 12 4 G1000 System Message Advisories 12 8 MFD amp PFD Alert Messages sssri 12 8 Database Alert Messages scesseesseessessseeseesesseaseean 12 9 TABLE OF CONTENTS GMA 1347 Alert Messages 12 10 GIA 63 Alert Messages 12 10 GEA 71 Alert Messages 12 12 GIX33 Alert Messages ire 12 13 GRS ZI Ale MESA ns 12 13 GMU 44 Alert Messages 12 14 GDL 69 Alert Messages 12 14 GDC 74A Alert Messages s sscsssesseessesseecsessseseeen 12 14 Miscellaneous Alert Messages ccssesseseeseesessen 12 14 on ne ou vo Index 1 Garmin G1000 Cockpit Reference Guide for the DA42 TABLE OF CONTENTS Blank Page IV Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 1 SYSTEM OVERVIEW
17. 259 voLTs 25 8 Voltmeter 79 LoaD 78 A a O as O PT Tachometer eee 1800 B 7 1200 ENGINE faa GEARBOX Gearbox 35 T 2330 RPM 2330 Temperature 4 Indicator Be pi EL COOLANT Coolant 2 C0 cPH 60 A i E Temperature OIL TEMP OT P SS Indicator ratur c s o Temperature indicator es Indicator 54 par 23 Oil Pressure FE DEICE FLUID oy Oil Pressure Y Deice Fluid i Indicator PR Indicator COOLANT TEMP Coolant k T Figure 3 2 SYSTEM Display TT Indicator Temperature M AE 3 3 FUEL DISPLAY Indicator FUEL QTY GAL eee Ae Quantity A NOTE If optional auxiliary fuel tanks are E rE e Indicator installed the fuel remaining can be adjusted up to a maximum of 76 4 gal the Fuel Quantity Figure 3 1 ENGINE Display Indicator does not account for fuel in the auxiliary tanks Garmin G1000 Cockpit Reference Guide for the DA42 3 1 SECTION 3 ENGINE INDICATION SYSTEM EIS Engine Load S Indicator oH 66 46 2H 72 LOAD 72 ohhh Bere a Tachometer 1866 1466 64 Fuel Quantity E Fuel Flow Indicator 4 8 Indicator Fuel T 55 Temperature FUEL CALC Indicator Gallons GAL REM 330 Remaining Gallons _ FPS s A Used ENDUR Mewes Endurance Range in Nautical i Sn ee Miles TTL TIME IN SVC Total Time GG GAG meee In Service Indicator Figure 3 3 FUEL Display I
18. Alert De icing fluid level is low 3 JF Single Aural Tone De icing pressure is low Stick limiting system has failed Annunciation Advisory Alerts Annunciation Window Text Alerts Window Message Audio Alert L R GLOW ON Left right engine glow plug active E No Tone L R FUEL XFER Left right fuel transfer from aux to main in progress Message Advisory Alerts TIS Voice Alerts The following voice alerts can be configured for Male or Female gender by using the Aux System Setup Page on the MFD Voice Alert Alert Trigger Traffic Played when a Traffic Advisory TA is issued Traffic Not Played when the traffic system fails or can Available not communicate 12 4 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 12 ANNUNCIATIONS amp ALERTS 12 3 G1000 SYSTEM ANNUNCIATIONS When an LRU or an LRU function fails a large red X is typically displayed on windows associated with the failed data The following section describes various system annunciations Refer to the Airplane Flight Manual for additional information regarding pilot responses to these annunciations NOTE Upon power up of the G1000 system certain windows remain invalid as G1000 equipment begins to initialize All windows should be operational within one minute of power up Should any window continue to remain flagged the G1000 system should be serviced by a Garmin authorized repair facility
19. 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 RX When a COM signal is received a white RX appears by the active COM frequency during signal reception e TX When a COM radio is transmitting 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 corresponding NAV radio is selected on the audio panel 118 640 com TX CON2 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 The percentage of maximum volume is displayed in place of the standby frequency selected by the tuning box COM1 135 675 35 VOLUME Figure 4 6 COM Volume Level 4 3 AUTOMATIC SQUELCH Automatic squelch can be disabled for a COM radio by pressing the COM Knob to place the tuning box on the desired COMS standby frequency then by pressing the VOL PUSH SQ Knob SECTION 4 NAV COM amp TRANSPONDER 4 4 QUICKLY ACTIVATING 121 500 MHZ Pressing and holding the COM Frequency Toggle Key
20. Intersections Page displayed press the FMS Knob to activate the cursor 2 Turn either FMS Knob to select the desired intersection 3 Press the FMS Knob to remove the flashing Cursor SECTION 7 NAVIGATION 7 10 NEAREST NDB 136 975 Figure 7 12 Nearest NDB Page Select the Nearest NDB Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the third rectangular page icon Access Information on a Specific NDB 1 With the Nearest NDB Page displayed press the FMS Knob to activate the cursor 2 Turn either FMS Knob to select the desired NDB The remaining information on the Nearest NDB Page pertains to the selected NDB 3 Press the FMS Knob to remove the flashing Cursor Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 7 NAVIGATION 7 11 NEAREST VOR Select the Nearest VOR Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the fourth rectangular page icon 136 975 ORTH UP 74 8 E7 EHH 17H 10 HH 11244 TIBNH TINH THFORHATTON Se PENDLETON PENDLETON OF fies HIGH ALTITUDE 20E D FREQUENCY EN sa a A 114 fel Figure 7 13 Nearest VOR Page View Information on the Nearest VOR 1 With the Nearest VOR Page displayed press the VOR Softkey to place the cursor in the NEAREST VOR box 2 Turn either FMS Knob to select a VOR 3 Press the FMS Knob to remove the fla
21. Map panning 10 5 Marker beacon 2 4 Messages 12 1 Message advisories 12 2 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 3 NAV2 5 3 Navigation 7 1 Navigation status window 2 2 NAV Frequency Window 4 1 Nearest Airports Page 7 3 7 5 7 7 1 8 7 9 8 1 Nearest ARTCC amp FSS frequencies 7 9 NEXRAD 10 3 10 4 10 7 O OBS 2 7 Obstacles 10 11 12 9 Operation 5 2 Operational E 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 RX indicator 4 3 R indication 4 5 S Severe thunderstorm 10 5 SIGMET 10 5 Slip Skid indicator 2 3 Softkey function MFD 1 4 1 6 Speed ranges 2 3 Split COM 5 1 5 2 Squelch 5 4 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 8 T TA 10 8 TAF 10 3 10 4 TAS 10 8 10 9 12 13 Terrain 10 10 12 9 Terrain proximity 10 8 Tornado 10 5 Traffic advisory 10 7 10 8 10 9 10 10 Traffic map page 10 7 10 8 10 9 10 10 10 11 Transponder 4 5 Transponder Status bar 4 5 Tropical storms 10 5 TX 4 3 V Vertical Deviation Glideslope indica tor 2 4 Vertical navigation profile 8 8 VER co
22. RSS Traffic Off Scale Traffic Banner Figure 10 14 TAS Traffic on Navigation Map in Non Bearing Traffic Advisories Avidyne TAS600 Series Refer to the Avidyne TAS600 Series Pilot s Guide for a detailed discussion of the TAS system and an explanation of the aural alerts Displaying Traffic on the Traffic Map Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page TAS OPERATING is displayed in the Traffic Mode field 3 Press the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the the BELOW NORMAL ABOVE or UREST unrestricted Softkey The selection is displayed in the Altitude Mode field Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 10 HAZARD AVOIDANCE 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area odh n Traffic Out of aircraft is 400 below rajjic Out o Traffic Mode Altitude Mode climbing Range 136 975 Non Bearing Traffic system is unable to determine bearing distance is 8 0 nm 1190 above and descending Proximity Traffic 1000 above amp descending Figure 10 15 Traffic Map Page Displaying Traffic on the Navigation Map 1 Ensure the TAS system is operating With the Navigation Map displayed press the MAP Softkey 2 Press the TRAFFIC Softkey Traffic will now be displa
23. When selecting an approach a GPS designation to the right of the procedure name indicates the procedure can be flown using the GPS receiver Some procedures will not have this designation meaning the GPS receiver can be used for supplemental navigation guidance only If the GPS receiver cannot be used for primary guidance the appropriate navigation receiver must be used for the selected approach e g VOR or ILS The final course segment of ILS approaches for example must be flown by tuning the Nav receiver to the proper frequency and selecting that Nav receiver on the CDI Load and or Activate an Approach Procedure 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 3 If no flight plan is active use the FMS Knobs to enter the identitier of the desired airport Press the ENT Key 4 Turn the large FMS Knob to highlight the Approach field Turn the small FMS Knob to display a list of available approaches Figure 9 6 Selecting an Approach Procedure Turn the FMS Knobs to highlight the desired approach Press the ENT Key Ul Garmin G1000 Cockpit Reference Guide for the DA42 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 op
24. a blank flight plan page for the first empty storage location STORED FLIGHT PLAN Figure 8 10 Create FPL on MFD Turn the small FMS Knob to display the Waypoint Information Window 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 steps 4 and 5 until the desired identifier has been entered WAYPOINT INFORMATION IDENT FACILITY CITY HOST RECENT LIST MAP pe he NORTH LP Figure 8 11 Waypoint Info Window Press the ENT Key Repeat steps 3 through 5 to enter the identifier for each additional flight plan waypoint 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 Press the FPL Key then press the FMS Knob to activate the cursor 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 Repeat step 2 to spell out the rest of the waypoint identifier Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint Repeat ste
25. by the annunciation LTNG lt 25 nm in the upper right corner _ NORTH UP LTNING OE Aas Figure 10 5 Lightning Display Range Annunciation To select cell or strike as the Stormscope lightning mode on the Navigation Map 1 From the Navigation Map Page press the MENU Key Select Map Setup and press the ENT Key 2 Turn the small FMS Knob to select Weather and press the ENT Key 3 Turn the large FMS Knob to select STRMSCP MODE 4 Turn either FMS Knob to display the Cell Strike Window 5 Turn either FMS Knob to select Cell or Strike Press the ENT Key 6 Push the FMS Knob to return to the Navigation Map Page To clear Stormscope lightning data from the Navigation Map Page 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight the Clear Lightning Data field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page Turn the large FMS Knob until the Map Page group is selected 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 St
26. for approximately two 2 seconds automatically tunes the selected COM radio to the emergency frequency 4 5 OPTIONAL NAV RADIOS ADF Radio optional To tune the ADF 1 Press the ADF DME Softkey and 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 transfer 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 MODE 4 ADF gt voL 507 DME MODE NAY ENT TO TRANSFER XPDR 1298 STBY LCL 16 52 54 ADF DME XPDR IDENT TMR REF NRST WARNING 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 The tuning window is displayed by pressing the ADF DME Softkey if no ADF is installed the softkey will be labeled DME ADF DME TUNING ADF 198 0 MODE4BFO vo 507 DME MODE MENA Figure 4 8 Radio Tuning Window To change the DME tuning source 1 1 2 4 4
27. highlight the 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 3 7 2 Press the Direct to 4 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 leg PAGE MENU OPT TONS Cancel Direct To NAV Press the FMS CRSR knob to return to bose page Figure 7 3 Canceling Direct to Navigation Direct to Navigation from the PFD WPT Symbol Identifier WPT Location Facility Name Flight Plan WPT Nearest WPT Bearing to WPT Distance from WPT Course to Selected WPT N 43 36 44 W119 44 26 ACTIVATE Lat Lon Figure 7 4 PFD Direct to Window Press the Direct to Key E 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 Press the Direct to G9 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 G10
28. key is stuck G S1 FAIL G S1 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 Alert Messages Alerts Window Message Comments GEA1 CONFIG GEA1 configuration The GEA 71 configuration settings do not match those of backup configuration error Contig service req d memory The G1000 system 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 The GEA 71 has incorrect sottware installed The G1000 system should be serviced 12 12 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 12 ANNUNCIATIONS amp ALERTS GTX 33 Alert Messages Alerts Window Message Comments o XPDR1 CONFIG XPDR1 contig error The transponder configuration settings do not match those of backup configuration Config service req d memory The G1000 system should be serviced MANIFEST GTX1 software mismatch The transponder has incorrect software installed The G10
29. 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 References 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 display 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 Pointer 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 traditional 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 Zero Figure 2 6 Attitude Indicator Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 2 FLIGHT INSTRUMENTS 2 3 ALTIMETER Altitude Alerting ae Reference Within 1000 ft Within 200 ft Deviation of 200 ft Ox
30. the cursor to the Frequencies box Turn either FMS Knob to scroll through the list placing the cursor on the desired frequency It a listed frequency has sector or altitude restric tions the frequency is preceded by an info i designation Press the ENT Key to view the information The following may be displayed with the frequency TX transmit only RX receive only PT part time frequency Press the ENT Key to place the selected fre quency in the standby field of the active COM or NAV To remove the cursor press the FMS Knob Garmin G1000 Cockpit Reference Guide for the DA42 1 3 SECTION 7 NAVIGATION 1 4 INTERSECTION INFORMATION Select the Intersection Information Page 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 1 4 With the Intersection Information Page displayed 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 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
31. when the next marker signal is received Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 5 AUDIO PANEL Marker Beacon Signal Sensitivity The HI SENS Key can be pressed for increased marker beacon signal sensitivity v v MKR HI MUTE SENS Figure 5 6 Navigation Radios Figure 5 5 Marker Beacon 5 5 INTERCOM SYSTEM ICS ISOLATION Press the PILOT and or COPLT Key to select who 3 4 NAV RADIO AUDIO SELECTION is isolated from hearing the Nav Com radios and music Pressing DME ADF NAVI or NAV2 selects and Selection scenarios are addressed in Table 5 1 deselects the radio source and activates the annunciator es Selected audio can be heard over the headset and the PILOT COPLT speakers These four keys can be selected individually ICS ISOLATION or together Figure 5 7 ICS Isolation PILOT KEY COPLT KEY Pilot Hears Copilot 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 OFF 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
32. 00 Cockpit Reference Guide for the DA42 Figure 7 5 Airport Information Page Select the Airport Information Page 1 2 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 With the Airport Information Page displayed 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 first character 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 6 SECTION 7 NAVIGATION a list is displayed from which to choose the desired location To remove the flashing cursor press the FMS Knob Access Runway Information With the Airport Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to place the cursor on the RUNWAYS identifier field Turn the small FMS Knob to display the next runway for the selected airport Continue turning the small FMS Knob to select the desired runway To remove the flashing cursor press the FMS Knob Access Frequency Information 5 With the Airport Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to move
33. 00 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 GRS 77 Alert Messages 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 any The AHRS is not receiving any or any useful GPS information Check AFMS limita GPS 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
34. Activate An Arrival Procedure 1 2 With the Navigation Map Page displayed press the FPL Key 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 If no flight plan is active use the FMS Knobs to enter the identifier of the desired airport Press the ENT Key Turn the large FMS Knob to highlight the Arrival field Turn the small FMS Knob to display a list of available arrivals 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 SECTION 9 PROCEDURES 9 2 6 A second window is displayed listing available transitions for the arrival Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key Figure 9 4 Select Arrival Transition 7 Athird window is displayed listing the available runways Turn the FMS Knobs to select the desired runway and press the ENT Key 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 airport and becomes part of the active flight plan If no flight plan is active when the arrival is loaded the arrival procedure will become the active flight plan 9 2 APPROACHES Not all approaches in the database are approved for GPS use
35. Bearing TO Distance Airport Symbol Identifier U56 Fs DE ETS VER MULTICOM 122 900 RNWY 35Q0QFT Runway Length KIDA 261 9 5NH ILS TOWER 118 500 RNWY 9 1FT KRXE 4 352 20 1NM YOR UNICON 122 800 RNWY 4200FT Primary COM Frequency Figure 7 10 Nearest Airports Window Press the NRST Softkey to display the PFD Nearest Airports Window View Information on a Specific Airport in the List 1 With the Nearest Airports Window displayed turn either FMS Knob to place the cursor on the desired airport identifier 2 Press the ENT Key to display airport information 3 Press the ENT Key again cursor is on BACK to return to the list Load an Airport COM Frequency into the Active COM 1 With the Nearest Airports Window displayed turn either FMS Knob to place the cursor on the desired airport trequency shown in the window 2 Press the ENT Key and the selected frequency will be placed in the COM standby frequency field 3 Press the Frequency Transfer Key to make the frequency the active frequency Garmin G1000 Cockpit Reference Guide for the DA42 1 9 EA anlai 136 975 NORTH UP wae SE eE E ARENI I 5 K Tey Figure 7 11 Nearest Intersections Page Select the Nearest Intersections Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the second rectangular page icon View Information on the Nearest Intersection 1 With the Nearest
36. COM input signal is recorded as the latest block Garmin G1000 Cockpit Reference Guide for the DA42 FLIGHT CONTROL SECTION 6 AUTOMATIC FLIGHT CONTROL Refer to the pilots guide for the installed autopilot system Garmin G1000 Cockpit Reference Guide for the DA42 6 1 SECTION 6 AUTOMATIC FLIGHT CONTROL Blank Page 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 the MAP Page Group 1 TRAFFIC Turn the large FMS Knob until MAP is highlighted in the Page Group Box 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 Dire
37. COM1 gt a gt COM2 Figure 5 2 Transceivers 5 2 SPLIT COM FUNCTION NOT RECOMMENDED ON THE DA42 NOTE Split COM performance is affected by the distance between the antennas and the separation of the tuned frequencies Figure 5 3 Split COM Function Pressing the COM 1 2 Key selects and deselects the split COM function During split COM operation the COMI COMI MIC COM2 and COM2 MIC Keys are active When the COM 1 2 Key is selected COM1 is used by the pilot for transmission and COM2 is used by the copi lot The COMI MIC annunciator blinks when the pilots Push to talk is pressed and the COM2 MIC annunciator blinks when the copilots Push to talk is pressed In this mode both the pilot and the copilot can trans mit simultaneously over separate radios The pilot can still monitor NAV1 NAV2 and MKR audio as selected but the copilot is only able to monitor COM2 5 3 MARKER BEACON RECEIVER The marker beacon receiver is always ON Figure 5 4 shows the marker beacon annunciators on the PFD Inner Marker Annunciator Middle Marker Annunciator Outer Marker Annunciator Figure 5 4 Marker Beacon Signal Indicator Lights on the PFD When the MKR MUTE Key is pressed the key annunciator 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
38. 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 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 Distance to Next Waypoint Next Waypoint Next Waypoint Current Track Figure 2 3 PFD Navigation Status Box 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 operating range normal operating range and never exceed speed Vne A red range is also present for low
39. DC 74A Air Data GIA 63s OR Computer DME ADF Source non hs Fin GIA 63 Integrated Avionics Units GDC 74A Air Data Computer GRS 77 AHRS Magnetometer GIA 63 Integrated Avionics Units ENT TO TRANSFER IDENT TMREREF NRST ALERTS GTX 33 Transponder OR GIA 63 Integrated Avionics Units Figure 12 5 G1000 System Failure Annunciations Garmin G1000 Cockpit Reference Guide for the DA42 12 7 SECTION 12 ANNUNCIATIONS amp ALERTS 12 4 G1000 SYSTEM MESSAGE ADVISORIES This section describes various G1000 system message advisories Certain messages are issued due to an LRU or an LRU function failure MFD amp PFD Alert Messages Message Comments S O DATA LOST Pilot stored data was The pilot profile data was lost System reverts to default pilot profile 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
40. Map Page Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the second rectangular page icon Press the OPERATE Softkey to begin displaying traffic TAS OPERATING is displayed in the Trattic Mode field Press the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the the BELOW NORMAL ABOVE or UREST unrestricted Softkey The selection is displayed in the Altitude Mode field Press the STANDBY Softkey to place the system in the Standby mode TAS STANDBY will be displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Garmin G1000 Cockpit Reference Guide for the DA42 Traffic Advisory aircraft is 400 a Trafic Out of Traffic Mode Altitude Mode climbing Range 118 008 core EL OPERATE ME Non Bearing Traffic system Proximity Gai is unable to determine bearin 1000 ab above amp distance is 8 0 nm 1190 above descending and descending Figure 10 13 Traffic Map Page Displaying Traffic on the Navigation Map 1 Ensure the KTA 870 system is operating With the Navigation Map displayed press the MAP Softkey 2 Press the TRAFFIC Softkey Traffic will now be displayed on the map SECTION 10 HAZARD AVOIDANCE Traffic Advisory ne NAVIGATION HAP 136 975 116 008 conz Ho NORTH UP Non Threat GES
41. Message Comments o GIA1 CONFIG GIA configuration error Contig service req d The GIA1 and or GIA2 configuration settings do not match backup configuration GIA2 CONFIG GIA2 configuration memory The G1000 system should be serviced error Contig service req d GIA1 COOLING GIAT temperature too low The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to GIA2 COOLING GIA2 temperature warm up to operating temperature too low GIA1 COOLING GIA1 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 GIA2 COOLING GIA2 over system should be serviced temperature GIA1 SERVICE GIA needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 GIA2 SERVICE GIA2 needs service system should be serviced Return the unit for repair 12 10 Garmin G1000 Cockpit Reference Guide for the DA42 GIA 63 Alert Messages Cont SECTION 12 ANNUNCIATIONS amp ALERTS Alerts Window Message Comments S 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 Reducing transmitter power COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM needs service Return unit for repair COM1 PTT COM push to
42. O1 USROO2 and so on If the selected waypoint is to be placed elsewhere 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 Softkey To change the user waypoint name follow the procedure for modifying a user waypoint 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 Garmin G1000 Cockpit Reference Guide for the DA42 3 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 Starting WPT Ending WPT DEP TIME N GS FUEL FLOW FUEL ONBOARD FUEL STATS EFFICIENCY TOTAL ENDUR REH FUEL REH ENDUR FUEL REQ OTAL RANGE Figure 8 15 Trip Planning Page For Direct to planning press the WPTS Softkey and verify that the starting waypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Turn the FMS Knobs to enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint OR For point to point planning turn the FMS Knobs to enter the identitier of the starting waypoint Once the waypoints identif
43. Softkey to change from 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 SECTION 2 FLIGHT INSTRUMENTS e INTEG GPS information is either not present or is invalid for navigation use e WARN GPS detects a position error e SUSP Displayed when in OBS Mode indicating GPS waypoint sequencing is suspended Figure 2 19 GPS INTEG GPS SUSP LOC1 and VOR2 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 NOTE The OBS Softkey is only displayed when navigating an active leg using GPS Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 2 FLIGHT INSTRUMENTS Blank Page 2 8 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 3 ENGINE INDICATION SYSTEM EIS SECTION 3 ENGINE INDICATION 3 2 ENGINE SYSTEM DISPLAY SYSTEM EIS Engine Load 3 1 ENGINE DISPLAY Indicator In all cases green indicates normal operation yellow indicates caution and red indicates warning 88 Loany 80 Pressing the ENGINE Softkey makes available the aoe ay SYSTEM and FUEL Soitkeys which in turn provide access ee ies once to the System Display and the Fuel Display respectively eal Engine Load Te oe RPM ou ELECTRICAL 49 a
44. TION 12 ANNUNCIATIONS amp ALERTS Miscellaneous Alert Messages Cont Alerts Window Message Comments S O SLCT NAV Select NAV on CDI for The system notifies 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 TRAFFIC FAIL Traffic device has The G1000 is no longer receiving data trom the traffic system The traffic device failed should be serviced a Ete nthe 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 3 Active flight plan 8 2 ADF 1 4 ADVISORY 12 1 Advisory alerts 12 4 Age 10 6 AHRS 12 13 Aircraft alerts 12 3 AIRMET 10 5 Airport frequency 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 Alert message 12 8 2 16 Altitude mode 10 8 Altitude reference bug 2 4 Altitude trend vector 2 4 Altitude volume 10 8 ALT knob 1 3 Annunciations 12 1 Approaches 9 2 Approach activation 4 4 Approach markers Signal augmen
45. TOMATIC 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 Enter a Direct to Destination ser 7 1 Select a Direct to Destination to a Flight Plan Waypoint or Nearest Airport 1 1 To Re center the CDI to the Destination Waypoint 7 2 To Manually Define the Direct to Course 7 2 Canceling Direct to Navigation 7 2 Direct to Navigation from the PFD s 7 2 Cancelling Direct to Navigation 7 2 7 3 Airport Information 1 3 Select the Airport Information Page 7 3 Enter a Waypoint Facility Name or City Location 7 3 Access RUNWAY Information 1 3 Access Frequency Information 1 3 7 4 Intersection Information 7 4 Select the Intersection Information Page 7 4 Access Information on an Intersection 1 4 7 5 NDB Information 7 4 Select the NDB Information Page 7 4 View Information on a Specific NDB 7 4 Garmin G1000 Cockpit Reference Guide for the DA42 TABLE OF CONTENTS 1 6 VOR Information 7 5 Select the VOR Information Page cessesesecsesesseeen 7 5 Access Information on a VOR sess i 7 7 User Waypoint Information Page 7 5 7 8 Nearest Airports oo cscs 7 5 Nearest Airport Information on the MFD uu 7 5 Select the Nearest Airports Page 7 5 Access Information on a Specific Airport
46. VERTICAL SPEED REQUIRED Begin descent in 1 FPM 00 26 18 LEGEND TARGET ALTITUDE TOP OF DESCENT BOTTOM OF CLIMB FPL OOG Turn the small FMS Knob to display a list possible VNAV profile endpoints When using a flight plan the target reference waypoint itself can be specified from the waypoints contained in the flight plan By default the last waypoint Garmin G1000 Cockpit Reference Guide for the DA42 in the flight plan is selected Highlight the desired waypoint 9 Press the ENT Key 10 With the TARGET ALTITUDE field highlighted turn the small and large FMS Knobs to select the target altitude If the selected altitude is above the current aircraft altitude a profiled climb is created If the selected altitude is below the current aircraft altitude a protiled descent will be created 11 Press the ENT Key The cursor is now placed in the TARGET VERTICAL SPEED field The default profile utilizes a 400 foot per minute descent rate 12 To change the vertical speed turn the FMS Knobs to enter the desired vertical speed Press the ENT Key when finished With the profile set the vertical speed required VSR is displayed Expect the following to occur when using the vertical navigation feature At one minute prior to reaching the Bottom Of Climb or Top Of Descent point gray arc the message APPR VPROF Approaching VNAV Profile is displayed as a PFD alert The descent or climb angle
47. a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or 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 Garmin G1000 Cockpit Reference Guide for the DA42 WARNINGS
48. ablish a direct course to the selected destination specified by the identifier chosen from the active route or taken from the map pointer 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 cancels an entry or removes page menus 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 options 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 arrivals from the flight plan If a flight plan is used available 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 selected 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
49. also locks to prevent changes in speed from altering the profile If selected the vertical speed required VSR readout on the default NAV and map pages shows the desired vertical speed to maintain the proper descent or climb angle At 500 feet above or below for a climb the target altitude white arc an APPR TRG ALT Approaching Target Altitude message is provided The VSR readout on the Navigation Map Page is blanked out at this point SECTION 8 FLIGHT PLANNING ALERTS APPR VPROF Ea aane ER ANT kA profile MFD FAN FAIL The cooling fan PFD FAN FAIL The cooling fan for the MFD is inoperative for the PFD is inoperative Figure 8 17 Approaching VNAV Profile Message PFD ALERTS APPR TRG ALTE target altitude MFD FAN FAIL The cooling fan for the MFD is inoperative PFD FAN FAIL The cooling fan for the PFD is inoperative Figure 8 18 Approaching Target Altitude Message PFD To display map data on the Vertical Navigation Map Page press the MAP Softkey Press the TOPO TERRAIN or LING Softkey Press the same softkey to remove the displayed data from the Vertical Navigation Page VNAV Page Menu Options The VNAV messages are not enabled until the VNAV Messages On option is enabled from the VNAV Page Menu Options To display the page menu press the MENU Key with the VNAV Page displayed The VNAV Page Options Menu also allows the pilot to restore VNAV Page detaults Ga
50. an operation or complete data entry It is also used to confirm selections and information 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 hundreds Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 1 SYSTEM OVERVIEW 1 2 PFD SOFTKEYS TERRAIN Softkey ON Softkey OFF optional Nnoannonognanngo 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 Removes everything except the active flight plan TRAFFIC Press to display traffic on the inset map TOPO Press to display topographical data ie coastlines terrain rivers lakes and elevation scale on the inset map TERRAIN Press to display terrain information on the inset map STRMSCP optional Press to display the lightning data on the inset map within a 200 nm radius of the aircraft NEXRAD optional Press to display NEXRAD precipitation data on the inset map XM LTNG optional Press to display the XM Radio lightning data on the inset m
51. ap BACK Press to return to the previous level softkey configuration ALERTS Press to display the Alerts Window PFD Press to display the additional softkeys for additional configuration of the PFD METRIC Press to display the current and reference altitudes in meters in addition to feet Pressing the metric softkey also changes the barometric setting to hectopascals DFLTS Press to reset default settings on the PFD DME optional Press to display the DME Information Window BRG bearing Press to cycle through the following information NAVI 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 following 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 STD BARO Press to set the barometric pressure to 29 92 i
52. arest Frequencies Page page group 2 Turn the small FMS Knob to select the seventh 1 Turn the large FMS Knob to select the NRST rectangular page icon page group 2 Turn the small FMS Knob to select the sixth Airspace Alerts Box rectangular page icon If the projected course takes the aircraft inside an des ah Ahead Select and Load the Nearest ARTCC FSS or Weather displaye ha E teense pequenty e If the aircraft is within two nautical miles of an 1 With the Nearest Frequencies Page displayed airspace and the current course takes the aircraft press the ARTCC FSS or Wx Softkey to place inside Ahead lt 2 nm is displayed the cursor in the appropriate field e If the aircraft is within two nautical miles of an 2 Turn the FMS Knobs to select the desired facility airspace and the current course will not take the aircraft inside Within 2 nm is displayed e If the aircraft has entered an airspace Inside is displayed or frequency 3 Press the ENT Key to load the frequency into the COM frequency standby field 4 Press the FMS Knob to remove the flashing cursor Garmin G1000 Cockpit Reference Guide for the DA42 7 9 SECTION 7 NAVIGATION View Additional Details for a Listed Airspace 1 With the Nearest Airspace Page displayed press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to scroll through the list highlighting the desired airspace 3 Press the ALERTS Softkey to plac
53. ast data update Proximity Traffic at same Traffic 1600 above amp 1 Turn the large FMS Knob to select the Map is older ane altitude level De ae EL moving in the Page Group sec resultingin in the direction of the line direction of the line Coast mode Figure 10 11 Traffic Map Page Garmin G1000 Cockpit Reference Guide for the DA42 10 7 SECTION 10 HAZARD AVOIDANCE Displaying Traffic on the Navigation Map 10 8 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 whenever TIS service becomes unavailable 10 5 TRAFFIC ADVISORY SYSTEM TAS OPTIONAL Honeywell KTA 870 Refer to the Honeywell KTA 870 Pilots Guide for a detailed discussion of the KTA 870 system System Self Test Set the range to 2 6 nm Press the STANDBY Softkey Press the TEST Softkey Self test will take approximately eight seconds to complete When completed sucessfully traffic symbols will be displayed as shown in Figure 10 12 and a voice alert TAS System Test OK will be heard If the self test fails the system will revert to Standby mode and a voice alert TAS System Test Fail will be heard 136 975 Figure 10 12 Self Test OK Display Displaying Traffic on the Traffic
54. craft 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 transponder Mode Selection softkeys 2 Press the CODE Softkey to display the transponder 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 Box 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 VFR 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 7 77 Military interceptor operations code NEVER ENTER THIS CODE e 0000 Code for military use in the U S Flight ID Reporting If so configured the Flight ID may be entered in the Timer Reterence Window If configuration is set to SAME AS TAIL the aircraft tail number will always be displayed GLIDE Ur Vx Vy
55. ct is active the product symbol is displayed in the lower right of the screen e NEXRAD e Cloud Top Echo Top e XM Lightning e Cell Movement e SIGMETs AIRMETs e METARs e City Forecast e Surface Analysis e Freezing Levels e Winds Aloft e County Warnings e Cyclone Warnings display the weather products available for the current subscription A green box by the weather product means that it is available NOTE The DONE Softkey on the AUX XM INFORMATION Page is used to save the GDL 69 A activation data when the XM services are initially 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 eel 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 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 10 HAZARD AVOIDANCE 2 Turn the sma
56. ct 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 Alert Messages Alerts Window Message Comments S O 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 tind 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 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 12 ANNUNCIATIONS amp ALERTS Miscellaneous Alert Messages Cont Alerts Window Message Comments S 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 The 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 Verity user moditied procedures
57. ct to Window Enter a Direct to Destination 1 Press the Direct to G39 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 waypoint identifier 4 Press the ENT Key to confirm the identifier The Activate field is highlighted 5 Press the ENT Key to activate Select a Direct to Destination to a Flight Plan Waypoint or Nearest Airport 1 While navigating an active flight plan press the Direct to GE Key 2 Turn the large FMS Knob to highlight the FPL NRST WAYPOINT field Garmin G1000 Cockpit Reference Guide for the DA42 7 1 SECTION 7 NAVIGATION 3 4 5 Turn the small FMS Knob to display a list of waypoints or airports Continue turning the small FMS Knob to scroll through the list and highlight the desired waypoint or airport Press the ENT Key to confirm the selection Press ENT again to activate a Direct to To Re center the CDI to the Destination Waypoint Press the Direct to E Key followed by pressing the ENT Key twice If a missed approach point MAP is the current destination the approach will be canceled To Manually Define the Direct to Course 1 Press the Direct to Key and enter a waypoint as discussed in previous steps or to edit the active direct to Turn the large FMS Knob to
58. d In AUTOMATIC mode fuel onboard is provided by the entry made in GAL REM on the EIS System Page Garmin G1000 Cockpit Reference Guide for the DA42 8 SECTION 8 FLIGHT PLANNING 11 The flashing cursor moves to the calibrated airspeed field Turn the FMS Knobs to enter a calibrated airspeed Press the ENT Key when finished 8 20 VERTICAL NAVIGATION VNAV PAGE NOTE An active flight plan or Direct to must be entered in order to utilize VNAV NOTE VNAV is advisory only and cannot be coupled to the autopilot 4 20KT Create a Vertical Navigation Profile 1 2 3 8 8 Press the FPL Key Turn the small FMS Knob to select the third page icon Press the FMS Knob to activate the cursor DTK UP TERRAIN 10 FT 100 FT With the TARGET POSITION distance field highlighted turn the FMS Knobs to select the desired distance for Top Of Climb or Bottom Of Descent from the VNAV profile endpoint The default distance is 4 nm Press the ENT Key The cursor is now positioned over the Before and After field Turn the small FMS Knob to select whether the previously set distance is Before or After the endpoint Press the ENT Key The cursor is now placed over the VNAV profile endpoint field ARGET POSITION Before KHDN TARGET ALTITUDE 3000FT Above WPT TARGET VERTICAL SPEED 400FPH 4 200NM Figure 8 16 Vertical Navigation VNAV Page STATUS
59. d Flight ID capability 190 00406 02 Retormatted manual to new format Added deicing capability Updated Annunciations and Alerts 190 00406 03 Added XM Weather capability 190 00406 04 Added TAS capability Various clerical changes Revision Date of Revision Affected Pages A 12 05 i Index 2 Initial Release B 3 06 i Index 2 Removed Ryan 9900BX Added Avidyne TAS600 Series Added Auxillary fuel tank note to EIS section Made various clerical changes Garmin G1000 Cockpit Reference Guide for the DA42 RR 1 RECORD OF REVISIONS Blank Page 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 Softkeys 1 4 1 3 MFD Softkeys occas 1 6 1 4 MFD Page Groups 1 8 1 5 Backlighting 1 8 SECTION 2 FLIGHT INSTRUMENTS 2 1 2 1 Airspeed Indicator 2 3 D C IAGICMONR ES 2 3 SPle ed ROE area 2 3 Airspeed Trend Vector 2 3 Vspeed References 2 3 2 2 Attitude Indicator 0 0 0 ccs 2 3 2 3 AIMER on 2 4 Altitude Reference Bug 2 4 Altitude Trend Vector 2 4 Barometric Setting BOX 2 4 ANTICS ACHING ne 2 4 2 4 Vertical Deviation Glideslope Indicator 2 4 2 5 Marker Beacon Annunciations 2 4 2 6 Vertical Speed Indicator 0 ccc ces 2 5 2 7 Horizontal Situation Indicat
60. de 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 radio 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 unusual 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 If heading is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircratt 11 2 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 12 ANNUNCIATIONS amp ALERTS SECTION 12 ANNUNCIATIONS amp e ALERTS Softkey Annunciation When the Alerting System issues an alert the ALERTS Soitkey ALERTS is used as a flashing annunciation to acc
61. de 4 5 VHF 4 1 VOL PUSH ID 4 2 VOL PUSH SQ 4 2 4 3 Volume squelch 5 4 Vspeeds 2 3 W WARN 2 7 Warning 12 1 12 2 Weather data link page 10 4 Weather product symbol 10 6 Weather product symbols 10 6 Weather warnings 10 5 Wind direction 10 5 Wind speed 10 5 X XM weather 10 4 XPDR softkey 4 5 Garmin G1000 Cockpit Reference Guide for the DA42 GARMIN At ns gt aa lt 2004 2006 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 04 Rev B
62. dentifier The cursor is now in the REFERENCE WAYPOINTS field If desired the waypoint can be defined by a reference waypoint Turn the FMS Knobs to enter the position coordinates or the radial and distance from the reference waypoint Press the FMS Knob to remove the flashing Cursor Modify a User Waypoint With the User Waypoint Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to move the cursor to the desired field and turn the small FMS Knob to make changes Press the ENT Key to accept the changes Press the FMS Knob to remove the flashing Cursor Delete a User Waypoint 1 Select the User Waypoint Information Page and press MENU to display the User Waypoint Information Page Options or press the DELETE Softkey 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 Garmin G1000 Cockpit Reference Guide for the DA42 8 1 SECTION 8 FLIGHT PLANNING Create User Waypoints from the Navigation Map Page 1 With the Navigation Map Page displayed push the Joystick to activate the panning function The map pointer is displayed at the present aircraft position 2 Move the Joystick to place the pointer at the desired position 3 Press the ENT Key The User Waypoint Information Page is now displayed with the captu
63. e Flight Plan Confirmation EDIT A STORED 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 place the cursor in the desired locations for entering changes 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 With either the Active or Stored Flight Plan displayed press the FMS Knob to activate the Cursor Turn the large FMS Knob to select the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window Remove KCRQ OK or CANCEL Figure 8 14 Remove Waypoint Confirmation 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 Garmin G1000 Cockpit Reference Guide for the DA42 8 5 SECTION 8 FLIGHT PLANNING Ul 8 15 8 6 Once all changes have been made press the FMS Knob to remove the cursor 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 Press the INVERT Softkey Invert and activa
64. e the cursor in the AIRSPACE ALERTS field 4 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 With the Nearest Airspace Page displayed press the FREQ Softkey to place the cursor in FREQUENCIES field 2 Turn either FMS Knob to select the desired frequency 3 Press the ENT Key to load the frequency into the COM frequency standby field 4 Press the FMS Knob to remove the flashing cursor 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 2 Turn the large FMS Knob to select the WPT page group 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 NEW Softkey A waypoint is created at the current aircraft position Turn the small FMS Knob to enter first character of the waypoint name Turn the large FMS Knob to move the cursor to the next character field 8 SECTION 8 FLIGHT PLANNING Repeat steps 2 and 3 until the desired name is entered Press the ENT Key Press the ENT Key a again to accept the new waypoint i
65. ed 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 CELL MOV Pressing the CELL MOV Softkey shows storm cell movement by displaying an arrow pointing in the direction of predicted movement The display is updated every 12 minutes SIG AIR Pressing the SIG AIR Softkey shows SIGMET and AIRMET information The display is updated every 12 minutes METAR Press the METAR Softkey to graphically display 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 group of softkeys for additional weather control Map SECTION 10 HAZARD AVOIDANCE 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 display 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 increments After pressing the WIND Softkey press the softkey correspondin
66. ercial 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 Honeywell is a registered trademark of Honeywell International Inc Avidyne is a registered trademark of Avidyne Corporation March 2006 190 00406 04 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 a
67. for the DA42 5 3 SECTION 5 AUDIO PANEL 5 4 5 6 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ Key to light the annunciator Pressing the small VOL SQ Knob now toggles between volume and squelch adjustment by lighting VOL or SQ respectively wv MAN SQ PLAY wv cREW v PILOT COPLT ICS _ ISOLATION PILOT O PASS VOL Figure 5 8 Volume Squelch Control 5 7 DIGITAL CLEARANCE RECORDER AND PLAYBACK Fach reception of primary active COM audio is automatically recorded ina memory block When the 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 9 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
68. g 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 CYCLONE Pressing the CYCLONE Softkey shows the current location of cyclones hurricanes and tropical storms and their projected track at various time intervals The update rate is every 12 minutes Panning Information Weather Data Link Page 1 2 Push in the Joystick to display the panning arrow Move the Joystick to place the panning arrow on AIRMETS TFRs METARs or SIGMETs Press the ENT Key to display pertinent information Garmin G1000 Cockpit Reference Guide for the DA42 10 5 SECTION 10 HAZARD AVOIDANCE 10 6 for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that displays the text of the report Panning over an airport with METAR information does not 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 produ
69. ier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again turn the FMS Knobs SECTION 8 FLIGHT PLANNING to enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint OR For flight plan leg planning press the FPL 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 Selecting FPL 00 will display an active flight plan If an active flight plan is selected REM will be an available option to display planning data for the remainder of the flight plan NOTE The Page Mode must be set to MANUAL to perform the following steps Turn the large FMS Knob to highlight the departure time DEP TIME field 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 system 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 finishe
70. ifferent 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 Alert Messages 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 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 GIA 63 Alert Messages Alerts Window
71. 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 14 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 System Setup in the G1000 Pilots Guide for more details Bearing Pointers and Information Windows Pressing the PFD Softkey provides access to the BRG1 and BRG2 Softkeys The BRGI Pointer is a single line pointer The BRG2 Pointer is a double line pointer DME Information Bearing 1 Window Pointer Bearing 2 Pointer Bearing 1 Bearing 2 Information Information Window Window Figure 2 15 HSI with Bearing Information 2 6 Garmin G1000 Cockpit Reference Guide for the DA42 Distance to Bearing Source Waypoint REA Identifier OJC NAYI lt Bearing Pointer Source Icon Figure 2 16 BRG1 Information Window Distance to Bearing Source ET A Waypoint AE eric Pointer Bearing Icon Source Figure 2 17 BRG2 Information Window DME optional To display the DME Information Window press the PFD Softkey followed by the DME Softkey Figure 2 18 DME Information Window Navigation Source To change between navigation sources 1 Press the CDI
72. ll FMS Knob to select the Traffic Weather Product Expires After Map Page minutes SIGMETS AIRMET 3 Press the OPERATE Softkey to begin displaying traffic TIS OPERATIING is displayed in the CityForecasts Traffic Mode field County Warnings oo 4 Press the STANDBY Softkey to place the system Cyclone Warnings Oo in the Standby mode TIS STANDBY will be Echo Tops displayed in the Traffic Mode field Freezing Levels o o 5 Rotate the Joystick clockwise to display a larger METARS a area or rotate counter clockwise to display a ii is NEXRAD If data is not received for a period longer than 6 seconds 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 o the traffic display up to 60 seconds until the next data Oo reception If no data is received after 60 seconds traffic a ee will be removed from the display 10 4 TRAFFIC INFORMATION SERVICE TIS Traffic Advisory aircraft is 400 above amp Traffic out o Traffic Mode descending moving in the direction of the line Le j A NOTE If the G1000 is configured to use the optional Skywatch Traffic Advisory System TIS will not be available for use A NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page L
73. 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 Attempt 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 Alert Messages Alerts Window Message Comments MFD1 DB ERR MFD1 aviation database error exists The MFD and or PFD detected a failure in the aviation database Attempt to reload PFD1 DB ERR PFD aviation the aviation database It pr
74. nches of mercury 1013 hPa by pressing the METRIC Softkey BACK Press to return to the previous level softkeys ALERTS Press to display the Alerts Window 1 4 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 1 SYSTEM OVERVIEW OBS Press to select OBS mode on the CDI when CODE Press to display transponder code selection navigating by GPS only available with active leg softkeys 0 7 CDI Press to change navigation mode on the CDI 0 through 7 Press numbers to enter code between GPS VORI and VOR2 IDENT Press to provide special aircraft ADF DME optional Press to display the ADF DME position identification to Air Traffic Control Tuning Window ATC XPDR Press to display the transponder mode BKSP Press to remove numbers entered one selection softkeys at a time STBY Press to select standby mode BACK Press to return to the previous level ON Press to select mode A softkeys ALT Press to select altitude reporting mode IDENT Press to provide special aircraft position VFR Press to automatically squawk 1200 only identification to Air Traffic Control ATC in the U S A refer to ICAO standards for VFR BACK Press to return to the previous level codes in other countries softkeys A optional optional optional AA AR AR AAA AAA Press the BACK or OFF softkey to return to the top level softkeys Figure 1 3 PFD Softkey Flow Chart 1 PFD opti
75. nformation on the MFD Select the Nearest Airports Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the first rectangular page icon Access Information on a Specific Airport 1 With the Nearest Airports Page displayed press the APT Softkey to place the cursor in the NEAREST AIRPORTS field The first airport in the nearest airports list is highlighted Garmin G1000 Cockpit Reference Guide for the DA42 15 SECTION 7 NAVIGATION 1 6 2 Press the FMS Knob then turn the large FMS Knob to highlight the desired airport 3 Press the FMS Knob to remove the flashing Cursor Access Runway Information for the Selected Airport 1 With the Nearest Airports Page displayed press the RNWY Softkey to place the cursor in the RUNWAYS field 2 Turn the small FMS Knob to select the desired runway 3 Press the FMS Knob to remove the flashing Cursor Quickly Tune the COM Transceiver to a Nearby Airport Frequency 1 With the Nearest Airports Page displayed press the FREQ Softkey to place the cursor in the FREQUENCIES field 2 Turn either FMS Knob to select the desired frequency 3 Press the ENT Key The selected frequency is placed in the COM standby frequency field 4 Press the Frequency Transfer Key to place the frequency in the active field 5 Press the FMS Knob to remove the flashing Cursor Nearest Airports Information on the PFD
76. oblem 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 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 d
77. oggle 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 receiver 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 with the compass lubber line 5 Joystick Changes the map range distance top to bottom of map display when rotated Activates the map pointer when pressed 6 CRS BARO Knob The large knob sets the altimeter 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 transceiver Pressing this knob toggles the tuning cursor light blue box between the COM 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 destination waypoint and est
78. ompany an alert During the alert the ALERTS Softkey assumes a new label consistent with alert level WARNING CAUTION or ADVISORY Pressing the softkey annunciation acknowledges that the pilot is aware of the alert The softkey then returns to the previous ALERTS label The pilot can then press the ALERTS Softkey again to view alert text messages NOTE The Airplane Flight Manual Supplement supersedes information found in this document The G1000 Alerting System conveys alerts to the pilot using a combination of the following items 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 detects invalid data on the PFD display or the MFD if system is in reversionary mode Up to 12 annunciations can EE be displayed simultaneously A white horizontal line separates annunciations that are acknowledged from annunciations that are not yet acknowledged Acknowledged annunciations are always above the line Annunciations are displayed in order Pee en of priority from top to bottom The highest Red X priority annunciation is displayed at the top of the Annunciation Window System Annunciations Typically a large red X appears in a window when a related LRU fails or Annunciation Alerts Window The Alerts Window displays Window alert text messages Up to 64 prioritized alerts can be displayed in
79. onal Ca OS OS OO OO RS RS RE EN DD Press the DFLTS softkey to change the PFD Press the STD BARO or BACK softkeys metric values to standard to return to the top level softkeys Figure 1 4 PFD Softkey Flow Chart 2 Garmin G1000 Cockpit Reference Guide for the DA42 1 5 SECTION 1 SYSTEM OVERVIEW optional F Press the BACK softkey to return to the top level softkeys Press the BACK ry ry ry softkey to return to the top level softkeys CIE CT EE Ce Ce ee aes Figure 1 5 PFD Softkey Flow Chart 3 IDENT Press to provide special aircraft position identification to Air Traffic Control ATC TMR REF Press to display the Timer References Window NRST Press to display the Nearest Airports Window ALERTS Press to display the Alerts Window 1 3 MFD SOFTKEYS ENGINE Pressing this softkey makes available the SYSTEM and FUEL Softkeys which in turn access the System Display and the Fuel Display 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 STRMSCP optional Pressing this softkey displays removes Stormscope lightning data on the Navigation Map NEXRAD optional Pressing this softkey dis
80. onger GPS position is in error provides GPS based guidance DGRD GPS ACC GPS position 2 accuracy degraded amp RAIM unavailable GPS position accuracy has been degraded and RAIM is not available RAIM UNAVAIL RAIM is not available GPS1 FAIL GPS1 is inoperative GPS2 FAIL GPS2 is inoperative A failure has been detected in the GPS1 and or GPS2 receiver The receiver is unavailable The G1000 system should be serviced Garmin G1000 Cockpit Reference Guide for the DA42 12 11 SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63 Alert Messages Cont Alerts Window Message Comments S GPS1 SERVICE GPS1 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still GPS2 SERVICE GPS needs service be available The G1000 system should be serviced Return unit for repair NAV1 SERVICE NAV1 needs service Return unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still NAV2 SERVICE NAV2 needs service be available The G1000 system should be serviced Return unit for repair NAV1 RMTXFR NAV1 remote Ea transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cycle its operation If the problem persists NAV RMTXFR NAV2 remote the G1000 system should be serviced transfer
81. or HSI 2 5 CONSO IR RE nm es 2 6 Course Deviation Indicator CDI 2 6 Bearing Pointers and Information Windows 2 6 DME ROD GMI SR 2 7 Navigation OUTRE nn mienne 2 7 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 1 3 1 Engine Display 3 1 3 2 Engine System Display 3 1 3 3 FUEL Display ou cesses estes 3 1 SECTION 4 NAV COM AND TRANSPONDER 4 1 4 1 Radio Status Indications 4 3 4 2 NO UME tan 4 3 4 3 Automatic Squelch 4 3 4 4 Quickly Activating 121 500 MHz 4 3 4 5 Optional NAV Radios 0 ccccceeseeeeen 4 3 ADF Radio OPA ane tan 4 3 DME Radio optional 4 4 4 6 Frequency Auto tuning cc een 4 4 AO UNION ME PDA nn 4 4 Autotuning on the MED nn 4 4 TABLE OF CONTENTS 4 7 Transponder 4 5 Mode SClOCUON ne mine 4 5 Ground Mode Automatic 4 5 RODW SAS ns E 4 5 Coge See Tion nn ceca scents a nteassech dy 4 5 FINED RE DOL UNG cschiarseutesssuasereadetmcsannaamenss 4 5 SECTION 5 AUDIO PANEL 5 1 5 1 COM Radio Selection 5 2 5 2 Split COM Function Not recommended on the DA tue ne sante cn 5 2 5 3 Marker Beacon Receiver 5 2 Marker Beacon Signal Sensitivity c ssesessesseeseesseen 5 3 5 4 Nav Radio Audio Selection 5 3 5 5 Intercom System ICS Isolation 5 3 5 6 Intercom Squelch Control 5 4 5 7 Digital Clearance Recorder and Playback 5 4 SECTION 6 AU
82. ormscope Page Press the MODE Softkey The CELL and STRIKE Softkeys are displayed Press the CELL Softkey to display CELL data or press the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page Garmin G1000 Cockpit Reference Guide for the DA42 NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells To change the viewing mode between 360 and 120 Select the Stormscope Page Press the VIEW Softkey The 360 and ARC Softkeys are displayed Press the 360 Softkey to display a 360 viewing area or press the ARC Softkey to display a 120 viewing area Press the CLEAR Softkey to remove all Stormscope lightning data trom the display XM WEATHER OPTIONAL WARNING XM Weather is not intended to be used for hazardous weather penetration Weather information provided by XM Radio Service is approved only for weather avoidance not penetration Press the MAP Softkey Press the NEXRAD or XM LING Softkey to display the desired weather Press the applicable softkey again to remove weather data trom the Navigation Map Page SECTION 10 HAZARD AVOIDANCE TOPO TERRANI rz BACK Figure 10 7 Navigation Map Page Displaying NEXRAD Weather Displaying METAR and TAF information on the Airport Information Page To display METAR and TAF text on the Airport Informa
83. plays removes precipitation data on the Navigation Map XM LING optional Pressing this softkey displays removes XM Radio lightning data on the Navigation Map 1 6 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 1 SYSTEM OVERVIEW BACK Pressing this softkey displays the ENGINE and MAP top level softkeys DCLTR declutter Pressing this softkey removes map information in three levels optional Press the BACK softkey on this level to return to the top softkey level nn A J O Q O e G e 7 a a do N ER Press to return to the top softkey level optional optional optional SH D DAD DND NDNA iw INC FUEL nnn iw A The DONE softkey changes to UNDO when the checklist item is already checked my DN P Ca HR EC se Figure 1 6 MFD Softkeys 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 PED DSPL gt 0 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
84. ps 2 through 4 to enter the identitier for each additional flight plan waypoint Once all waypoints have been entered press the FMS Knob remove the cursor The new flight plan is now active Figure 8 12 Creating Flight Plan on the PFD Garmin G1000 Cockpit Reference Guide for the DA42 8 8 LOAD A DEPARTURE See the Procedures section for a discussion on loading and activating departure procedures 8 9 LOAD AN ARRIVAL See the Procedures section for a discussion on loading and activating arrival procedures 8 10 LOAD AN APPROACH See the Procedures section for a discussion on loading and activating approach procedures 8 11 REMOVE A DEPARTURE ARRIVAL OR APPROACH FROM A FLIGHT PLAN With the Active or Stored Flight Plan Page displayed press the FMS Knob to activate the cursor 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 Press the CLR Key to display a confirmation window With OK highlighted press the ENT Key to remove the selected procedure STORE A NEWLY CREATED FLIGHT PLAN After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key With OK highlighted press the ENT Key to store the flight plan SECTION 8 FLIGHT PLANNING Figure 8 13 Stor
85. rain Obstacle at or within 100 below current aircraft altitude CAUTION Terrain Obstacle between 100 and 1000 below current aircraft altitude rote Aircraft Altitude ee EL 4 100 Threshold Lighted Obstacle Height is less than 1000 AGL Unlighted Obstacle Height is greater than 1000 AGL Lighted Obstacle Height is greater than 1000 AGL Figure 10 18 Obstacle Symbols Garmin G1000 Cockpit Reference Guide for the DA42 10 11 SECTION 10 HAZARD AVOIDANCE Blank Page 10 12 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 11 ABNORMAL OPERATION 11 1 REVERSIONARY MODE Should a system detected failure occur in either display the G1000 automatically enters reversionary mode In reversionary mode critical 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 activated 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 reversionary mode NOTE The Airplane Flight Manual always takes precedence over the information found in this section Normal MFD Display MFD in Reversionary Mo
86. red position 4 Turn the FMS Knobs to select a waypoint Figure 8 3 Active Flight Plan Page on the MFD name 5 Press the ENT Key to accept the selected 8 3 ACTIVATE A STORED FLIGHT PLAN name The first reference waypoint field is Press the FPL Key and turn the small FMS Knob highlighted to display the Flight Plan Catalog Page 6 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 7 Press the FMS Knob to remove the flashing Cursor 8 2 VIEWING THE ACTIVE FLIGHT PLAN Press the FPL Key Figure 8 4 Flight Plan Catalog Page KSTL Meet A AN y 2 Press the FMS Knob to activate the cursor MOODS iof 127 19 3 Turn the large FMS Knob to highlight the desired Figure 8 2 Active Flight Plan Window on the PFD 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 2 Garmin G1000 Cockpit Reference Guide for the DA42 8 4 ACTIVATE A FLIGHT PLAN LEG 1 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired destination waypoint 2 Press the ACT LEG Softkey using MFD only OR 3 Press the MENU Key select the Activate Leg option trom the page menu and p
87. ress the ENT Key This step must be used when activating a leg from the PFD 4 With Activate highlighted press the ENT Key KIAH Course 236 from KOJE to KIAB ACTIVATE or CANCEL 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 6 Delete Flight Plan 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 SECTION 8 FLIGHT PLANNING the flight plan This will not delete the stored flight plan only the active flight plan Figure 8 7 Delete Flight Plan Confirmation INVERT ACTIVE FLIGHT PLAN From the Active Flight Plan Page press the MENU Key to display the Page Menu Turn the large FMS Knob to highlight Invert Flight Plan and press the ENT Key The original flight plan remains intact in its flight plan catalog storage location With OK highlighted press the ENT Key to invert the flight plan Figure 8 9 Invert Flight Plan Confirmation Garmin G1000 Cockpit Reference Guide for the DA42 8 3 SECTION 8 FLIGHT PLANNING 8 4 8 1 CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the MFD 1 2 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Press the NEW Softkey to display
88. rmin G1000 Cockpit Reference Guide for the DA42 8 9 SECTION 8 FLIGHT PLANNING Blank Page 8 10 Garmin G1000 Cockpit Reference Guide for the DA42 9 1 SECTION 9 PROCEDURES ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1 2 With the Navigation Map Page displayed press the FPL Key Press the LD DP Softkey If a flight plan is active the departure airport will be displayed as the default A list of available departures is also displayed If no flight plan is active use the FMS Knobs to enter the identifier of the desired airport Press the ENT Key Turn the large FMS Knob to highlight the Departure field Turn the small FMS Knob to display a list of available departures Turn either FMS Knob to select the desired departure and press the ENT Key AIRPORT KIND y PUBLIC HEH CENTURY ATRCENTER OLATHE KS DEPARTURE CHIEFS Figure 9 1 Select Departure A list of runways may be displayed for the departure Turn the FMS Knobs to select the desired runway and press the ENT Key A list of available transitions is displayed for the departure Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key 8 SECTION 9 PROCEDURES DEPARTURE CHIEFS RUNWAY ALL TRANSITION CATTS Figure 9 2 Select Departure Transition With LOAD highlighted press the ENT Key The departure will be active when the flight plan is active Load and
89. s the FMS CRSA knob to return to bose poge Figure 10 1 Page Menu HAP SETUP STRHSCP LTNG n STRHSCP HODE Cal 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 The Stormscope system is not intended to be used for hazardous thunderstorm penetration Weather information on the G1000 MFD is approved for weather avoidance only Refer to the WX 500 Pilot s Guide for detailed operation 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 ial Eat 136 973 TET NORTH 4 LINING AH PARR JERO HLG Figure 10 4 In Flight Navigation Map Page Displaying Stormscope Lightning Data Lightning Age Strike is less than 6 seconds old 4 ay dh 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 10 2 At a map range of less than 25 nm Stormscope lightning data is not displayed but can still be present The presence of Stormscope lightning data is indicated
90. shing Cursor Select and Load a VOR Frequency 1 With the Nearest VOR Page displayed press the FREQ Softkey to highlight the VOR frequency in the FREQUENCY field 2 Press the ENT Key The selected VOR frequency is placed in the NAV standby frequency field 3 Press the FMS Knob to remove the flashing Cursor 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 displayed press the FMS Knob to activate the cursor It any previously entered User Waypoints are within 200 nm these will be displayed with the closest listed first 2 Turn either FMS Knob to select the desired waypoint The remaining information on the Nearest User Waypoint Page pertains to the selected Nearest User Waypoint 7 8 Garmin G1000 Cockpit Reference Guide for the DA42 SECTION 7 NAVIGATION 3 Press the FMS Knob to remove the flashing 7 14 NEAREST AIRSPACES cursor ST NEAREST ARE 136 975 NORTH UP ATRGPACE IRSPACE ALERTS 1 13 NEAREST FREQUENCIES 7 95 EN 136 975 Ri Di F i h ADC oe ANT CA ne DT ES NEAREST ARTCC Ln VW f 3 e Se AT TI F Figure 7 16 Nearest Airspaces Page Select the Nearest Airspaces Page i a rage 1 Turn the large FMS Knob to select the NRST Select the Ne
91. t desired use the DEC FUEL INC FUEL and RST FUEL Soitkeys to adjust the amount of fuel remaining for totalizer calculations NOTE Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset 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 boxes are located on the Primary Flight Display and the Multi Function Display in the same locations NAV COM Controls NAV Frequency Box COM Frequency Box Controls nevi 13 25 110 90 er ESTI ns 1991 295 mk 095 118 900 133 808 con 119 90 124 308 135 325 cz 1000 PUSH 1 2 CRS 4 BARO PUSH CAS CTA 650A RANGE M E iki 15TH H Ll INSET FD CD OBS XPDR IDENT TMR REF HRST Figure 4 1 G1000 VHF NAV COM Interface PFD Garmin G1000 Cockpit Reference Guide for the DA42 4 1 SECTION 4 NAV COM amp TRANSPONDER Standby NAV Selected NAV Selected COM Standby COM Frequency Field Frequency Frequency Frequency Field nav1 189 98 gt 110 60 Cv ee RE EE RER Figure 4 2 Frequency Fields Tuning Box Active NAV Active COM Tuning Box Frequency Field Frequency Field 135 166 COM 600 121 990 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
92. t may require pilot intervention A caution alert is accompanied by an annunciation in the ADVISORY Annunciation Window Caution text appearing in DVI SURY the Annunciation Window is YELLOW A caution Figure 12 4 ADVISORY Softkey alert is also accompanied by a flashing CAUTION Annunciation Softkey 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 Annunciation 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 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
93. talk key is stuck COM2 PTT COM2 push to talk key is stuck COM1 RMT XFR COM1 remote transter Key is stuck COM2 RMT XFR COM remote transfer key is stuck RAIM UNAVAIL RAIM is not available trom FAF to MAP waypoints 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 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 POSN ERROR RAIM has determined When a RAIM position error is detected GPS is flagged and the system no l
94. tation 5 3 Arrivals 9 1 Attitude indicator 2 3 Audio panel 4 3 5 1 Audio panel controls ADF 5 3 COM 1 2 5 2 DME 5 3 NAV1 5 3 NAV2 5 3 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 5 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 4 Create a new user waypoint 8 1 Cyclones 10 5 Cylinder select 3 2 D Departures 9 1 Direct to 7 1 DME 1 5 Dual CDU failure 11 2 E ECHO TOPS 10 5 Edit a flight plan 8 5 Emergency code 4 5 Engine display 3 1 ENGINE softkey 3 1 F Flight ID 4 5 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 2 G GMA 1347 1 1 Heading indication 2 6 Headset s 5 3 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 INTEG 2 7 Interrogations 4 5 K Key s 1 3 L Lightning 10 2 10 3 10 5 Load approach 8 5 Load a VOR frequency 7 8 Load departure 8 5 Load the frequency for a controlling agency 7 10 Load the nearest ARTCC frequency 7 9 Loss of communication code 4 5 Garmin G1000 Cockpit Reference Guide for the DA42 Index 1 MAP 7 1
95. te stored flight plan will be displayed With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location COPY A FLIGHT PLAN 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 Press the COPY Softkey 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 DELETE A FLIGHT PLAN 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 Press the DELETE Softkey 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 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 waypoint will be inserted at the end of the flight plan The default user waypoint naming is USROOO USRO
96. ter Figure 2 10 Vertical Speed Indicator The actual vertical speed is displayed inside the pointer 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 11 Horizontal Situation Indicator Garmin G1000 Cockpit Reference Guide for the DA42 2 5 SECTION 2 FLIGHT INSTRUMENTS Turn Rate Indicator and Heading Trend Vector Tick marks to the left and right of the lubber line denote halt standard and standard turn rates A magenta turn rate trend vector shows the current turn rate The end of the trend vector gives the heading predicted in six seconds based on the present turn rate At rates greater than 4 deg sec an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid Half Standard Turn Rate Tick Mark D Rae Standard Turn BORN Trend Vector Rate Tick Mark rate gt 4 Turn Rate Trend Vector standard rate Figure 2 13 Standard Rate Turn Indication Course Pointer The Course Pointer is a single
97. the Alerts Window Pressing A E the ALERTS Softkey displays the Alerts Window ALTERNATOR Alternator failed Pressing the ALERTS Softkey again removes the Battery is only elec source gg Alerts Window Alerts Window from the display When the Alerts peed ae Ta e St Window is displayed the pilot may use the large PITOT OFF Pitot heat is off FMS Knob to scroll through the alert list Higher Por 1200 ALT LCL OO priority alerts are displayed at the top of the window RESTE ALERTS Softkey Lower priority alerts are displayed at the bottom of Figure 12 1 G1000 Alerting System anes the window 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 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 existence of abnormal conditions on the aircraft tha
98. tion 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 information is updated every 12 minutes Garmin G1000 Cockpit Reference Guide for the DA42 10 3 SECTION 10 HAZARD AVOIDANCE 136 975 COMZ NORTH UP aTRPORT WU KMP PUBLIC MINNEAF POLIS ST PAUL INTL MINNEAPOLIS MN NORTH UP METAR HIND D Pa 240 ISIBIL METAR AGET FEW an Text SHBHFT BROKEN 2oHIBAFT BRO EN DEH POINT 14 E ALTIMETER 29 721N TAF Text CELL MOV SIO ATR PETAR LEGEND HORE WK Wx Figure 10 9 Weather Data Link Page Softkey 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 Figure 10 8 METAR and TAF Text Displayed on the Airport Weather Information Page Displaying Weather on the Weather Data Link Page To select the Weather Data Link Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather NEXRAD base reflectivity does not provide Data Link Page sufficient information to determine cloud layers or precipitation characteristics hail vs rain etc
99. tion assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course Figure 9 7 Selecting an Approach Transition 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 With the Navigation Map Page displayed press the PROC Key Turn the large FMS Knob to highlight ACTIVATE APPROACH Press the ENT Key The approach procedure is now active SECTION 9 PROCEDURES Garmin G1000 Cockpit Reference Guide for the DA42 9 3 SECTION 9 PROCEDURES Blank Page 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 Pres
100. voidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated 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 navigational 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 is not intended for hazardous weather penetration thunderstorm penetration Stormscope information as displayed on the G1000 MFD is to be used only for
101. weather avoidance not penetration WARNING GDL 69 Weather should not be used for hazardous weather penetration Weather information provided by the GDL 69 is approved only for weather avoidance not penetration Garmin G1000 Cockpit Reference Guide for the DA42 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 functional 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
102. yed on the map see Figure 10 14 10 6 Displaying Terrain and Obstacles on the Terrain Proximity Page TERRAIN AND OBSTACLE PROXIMITY NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south 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 cor 20KT HOG UF Figure 10 16 Terrain Proximity Page 10 10 Garmin G1000 Cockpit Reference Guide for the DA42 ELEV FT MAX 1817 HIN 577 Maximum elevation of topography presently isplayed on screen SECTION 10 HAZARD AVOIDANCE Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed press the Aull a ri j nie of topograp leva tion o dis played on screen Unlighted Obstacle Height is less than 1000 AGL eatin of MAP Softkey tly disp Bee 2 _ Press the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map Aircraft altitude Ground elevation at present aircraft position WARNING Ter

Garmin Software Version 0370.14 Cockpit Reference Guide

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