G1000 TM Cockpit Reference Guide for the Diamond DA42
Copyright © 2004, 2005 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0370.13 or later for the DA42. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.3411 Fax 503/364.
WARNINGS, CAUTIONS, & 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.
WARNINGS, CAUTIONS, & 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.
WARNINGS, CAUTIONS, & 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.
WARNINGS, CAUTIONS, & NOTES This page intentionally left blank.
RECORD OF REVISIONS Part Number 190-00406-00 190-00406-01 Change Summary Initial Release Added DME capability Added BRG1/BRG2 pointers Changed Airspeed Trend Vector Changed Altitude Trend Vector Added Checklist capability Added Flight ID capability 190-00406-02 Reformatted manual to new format Added deicing capability Updated Annunciations and Alerts 190-00406-03 Added XM Weather capability Added TAWS-B Updated Message Advisories Added Lycoming engine parameters.
RECORD OF REVISIONS This page intentionally left blank.
TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW .................................. 1-1 PFD/MFD Controls................................................... 1-2 PFD Softkeys............................................................ 1-4 MFD Softkeys .......................................................... 1-7 MFD Page Groups ................................................... 1-8 Backlighting ............................................................. 1-8 4.7 Transponder ...................................
TABLE OF CONTENTS 7.9 Nearest Intersections ............................................ 7-6 Select the Nearest Intersections Page........................... 7-6 View Information on the Nearest Intersection .............. 7-7 7.10 Nearest NDB ............................................................ 7-7 Select the Nearest NDB Page ....................................... 7-7 Access Information on a Specific NDB .......................... 7-7 7.11 Nearest VOR ................................................
TABLE OF CONTENTS 11.4 Stormscope Operation with Loss of Heading Input........................................................ 11-2 SECTION 12: ANNUNCIATIONS AND ALERTS ...... 12-1 12.1 Alert Level Definitions ........................................ 12-2 12.2 Aircraft Alerts ........................................................ 12-3 WARNING Alerts ....................................................... 12-3 CAUTION Alerts ........................................................
TABLE OF CONTENTS This page intentionally left blank.
SECTION 1 SYSTEM OVERVIEW SECTION 1: SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operating guide.
SECTION 1 SYSTEM OVERVIEW 1.
SECTION 1 SYSTEM OVERVIEW (1) NAV VOL/ID Knob – Controls the NAV audio level. Press to toggle the Morse code identifier ON and OFF. Volume level is shown in the field as a percentage. (2) NAV Frequency Toggle Key – Toggles the standby and active NAV frequencies. (3) Dual NAV Knob – Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the NAV receiver. Press to toggle the tuning cursor (light blue box) between the NAV1 and NAV2 fields.
SECTION 1 SYSTEM OVERVIEW 1.2 PFD SOFTKEYS Softkey ON Softkey OFF (optional) INSET PFD OBS CDI ADF/DME XPDR IDENT TMR/REF NRST ALERTS 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.
SECTION 1 SYSTEM OVERVIEW STD BARO – Press to set the barometric pressure to 29.92 inches of mercury (1013 hPa by pressing the METRIC softkey). BACK – Press to return to the previous level softkeys. OBS – Press to select OBS mode on the CDI when navigating by GPS (only available with active leg).. CDI – Press to change navigation mode on the CDI between GPS NAV1 and NAV2. ADF/DME (optional) – Press to display the ADF/DME Tuning window. XPDR – Press to display the transponder mode selection softkeys.
SECTION 1 SYSTEM OVERVIEW PFD (optional) DFLTS METRIC DME 360 HSI BRG1 ARC HSI BRG2 STD BARO BACK ALERTS Press the STD BARO or BACK softkeys to return to the top level softkeys Press the DFLTS softkey to change the PFD metric values to standard Figure 1-4 PFD Softkey Flow Chart – 2 (optional) OBS .
SECTION 1 SYSTEM OVERVIEW 1.3 MFD SOFTKEYS STRMSCP (optional) – pressing this softkey displays/removes Stormscope lightning data on the Navigation Map. NEXRAD (optional) – pressing this softkey displays/removes precipitation data on the Navigation Map. XM LTNG (optional) – pressing this softkey displays/removes XM Radio lightning data on the Navigation Map. BACK – pressing this softkey displays the ENGINE and MAP top level softkeys.
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 Group Waypoint Page Group Map Page Group Selected Page Figure 1-7 Page Group Icon 1.5 BACKLIGHTING To manually adjust the backlight for the PFD and MFD: 1-8 1. Press the MENU key on the PFD to display the PFD Setup Menu window. 2.
SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display, unless otherwise indicated.
SECTION 2 FLIGHT INSTRUMENTS 11 1 10 9 2 8 3 7 4 5 6 1 Traffic Annunciation 7 Alerts Window 2 Selected Heading Box 8 Selected Course Box 3 Inset Map 9 Annunciation Window 4 BRG1 Information Window 10 Vertical Deviation/Glideslope Indicator 5 DME Information Window 11 Marker Beacon Annunciation 6 BRG2 Information Window Figure 2-2 Additional PFD Information Distance to Next Waypoint Next Waypoint Desired Track to Next Waypoint Current Track Figure 2-3 PFD Navigation Status Wi
SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Vspeed References Airspeed Trend Vector Vyse (Blue Line) Actual Airspeed Vspeed References Vmc (Red Line) Speed Ranges True Airspeed Box Figure 2-4 Airspeed Indicator Speed Indication The indicated airspeed is displayed inside the black pointer. The pointer will become red upon reaching Vne. Vspeed References are turned on or off in the Timer/References window. Press the TMR/REF softkey to display the widow.
SECTION 2 FLIGHT INSTRUMENTS 2.3 ALTIMETER Barometric Setting Box Altitude Reference Box To set barometric pressure, turn the BARO knob to select the desired setting. 2.4 Altitude Trend Vector Current Altitude The Vertical Deviation/Glideslope Indicator appears when an ILS is tuned in the active NAV field. 2.
SECTION 2 FLIGHT INSTRUMENTS 2.6 VERTICAL SPEED INDICATOR 14 13 1 Vertical Speed Pointer 12 2 11 3 10 4 9 8 5 7 6 Figure 2-9 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 Turn Rate Indicator and Heading Trend Vector Bearing Pointers and Information Windows Each tick mark is at 9 (half standard rate tick mark) and 18 (standard rate tick mark) degrees to the left and right of the lubber line. A wide magenta line displays the current turn rate, up to 24 degrees. A magenta arrowhead appears at 25 degrees. This trend vector provides the pilot with a prediction of what the heading will be in 6 seconds at the present turn rate.
SECTION 2 FLIGHT INSTRUMENTS DME Radio (optional) To display the DME Information Window, press the PFD softkey followed by the DME softkey. Figure 2-17 DME Information Window Navigation Source To change between navigation sources: 1. Press the CDI softkey to change from GPS to VOR1/LOC1. 2. Press the CDI softkey again to change from VOR1/LOC1 to VOR2/LOC2. Press the CDI softkey a third time to return to GPS. • INTEG – RAIM is not available • WARN – GPS detects a position error 3.
SECTION 2 FLIGHT INSTRUMENTS . This page intentionally left blank.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) SECTION 3: ENGINE INDICATION SYSTEM (EIS) 3.1 3.2 FUEL DISPLAY Engine Load Indicator ENGINE DISPLAY In all cases green indicates normal operation, yellow indicates caution, and red indicates warning. Tachometer Pressing the ENGINE softkey makes available the SYSTEM and FUEL softkeys which in turn provide access to the System Page and the Fuel Page, respectively.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.
SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER The Nav/Com controls and frequency windows are located on the Primary Flight Display and the Multi-Function Display in the same locations.
SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Tuning Box Selected NAV Frequency Active NAV Frequency Field Navigation Status Window Selected COM Frequency Figure 4-2 Frequency Fields Frequency Toggle Arrow Active COM Frequency Field Tuning Box Figure 4-3 Frequency Toggle Arrow and Tuning Box NAV Controls COM Controls VOL/PUSH ID Knob VOL/PUSH SQ Knob Frequency Toggle Key Dual NAV Knob Dual COM Knob • Turn to tune in desired frequencies.
SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS • TX – When a COM radio is keyed, a white TX indication appears to the right of the corresponding COM frequency. • ID – When the Morse code identifier is ON for a NAV radio, a white ID indication appears to the left of the corresponding active NAV frequency. The Morse code identifier can be heard if the corresponding NAV radio is selected on the audio panel. Figure 4-5 Radio Status Indications 4.
SECTION 4 – NAV/COM & 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). Auto-tuning on the PFD Figure 4-8 Radio Tuning Window To change the DME tuning source: FREQUENCY AUTO-TUNING Figure 4-10 Nearest Airports Window (PFD) 1. Press the NRST softkey to display the Nearest Airports Window. 1. From the Tuning window, turn the large FMS knob to highlight the DME source field. 2. 2.
SECTION 4 – NAV/COM & TRANSPONDER 4.7 TRANSPONDER Following is a list of important codes: Mode Selection The STBY, ON and ALT softkeys can be accessed by pressing the XPDR softkey. Ground Mode (Automatic) GND is displayed when the aircraft is on the ground. Figure 4-11 Ground Mode Reply Status When the transponder sends replies to interrogations, an “R” indication appears momentarily in the reply status field. • 1200 – VFR code in the U.S.
SECTION 4 – NAV/COM & TRANSPONDER This page intentionally left blank.
SECTION 5 – AUDIO PANEL SECTION 5: AUDIO PANEL Transceiver Audio (COM 3 is unavailable) Transmitters (COM3 MIC is unavailable) Split COM (Unavailable) Telephone (Unavailable) Passenger Address Speaker Marker Beacon/Mute Marker Beacon Signal Sensitivity Aircraft Navigation Radio Audio (ADF & DME optional, AUX unavailable) Manual Squelch Aircraft Navigation Radio Audio Recorded COM Audio Playback ICS Isolation VOL/SQ Volume/Squelch VOL Annunciation SQ Annunciation Reversionary Mode Figure 5-1
SECTION 5 – AUDIO PANEL 5.1 COM RADIO SELECTION Marker Beacon Signal Sensitivity Pressing the COM1 MIC or COM2 MIC key selects the active transmitter (i.e., microphone). The associated receiver audio (COM1 or COM2) also becomes selected when the COM MIC key is pressed. To prevent deselecting the desired received audio when pressing another COM MIC key, press the already selected COM1 or COM2 key before pressing the other COM MIC key. Figure 5-4 Marker Beacon 5.
SECTION 5 – AUDIO PANEL 5.5 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ key to light the annunciator. Figure 5-5 Navigation Radios 5.4 INTERCOM SYSTEM (ICS) ISOLATION Pressing the small VOL/SQ knob now toggles between volume and squelch adjustment by lighting VOL or SQ respectively. Press the PILOT and/or COPLT key to select who is isolated from hearing the Nav/Com radios and music. Selection scenarios are addressed in Table 5-1.
SECTION 5 – AUDIO PANEL 5.6 DIGITAL CLEARANCE RECORDER WITH PLAYBACK CAPABILITY Each reception of primary active COM audio is automatically recorded in a memory block. When the next transmission is received, it is recorded in the next 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.
SECTION 6 – AUTOMATIC FLIGHT CONTROL SECTION 6: AUTOMATIC FLIGHT CONTROL Refer to the pilot’s guide for the installed autopilot system.
SECTION 6 – AUTOMATIC FLIGHT CONTROL This page intentionally left blank.
SECTION 7 – NAVIGATION SECTION 7: NAVIGATION The following discussions pertain to the Multi-function Display, unless otherwise indicated. 7.1 NAVIGATION MAP PAGE 7.2 DIRECT-TO NAVIGATION Direct-to Navigation from the MFD Identifier Facility Name City Symbol Nearest Airport Flight Plan Field Select the MAP Page Group Map Orientation 1. Turn the large FMS knob until MAP is highlighted in the page group window in the lower right of the MFD display. 2.
SECTION 7 – NAVIGATION 4. 5. 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 (HSI) needle to the same destination waypoint: 1. ) key, followed by Press the Direct-to ( pressing the ENT key twice. NOTE: If a missed approach point (MAP) is the current destination, the approach will be canceled.
SECTION 7 – NAVIGATION 7.3 AIRPORT INFORMATION 7. To remove the flashing cursor, press the FMS knob. Access Runway Information 1. Press the FMS knob to activate the cursor. 2. Turn the large FMS knob to place the cursor on the Runways field. 3. Turn the small FMS knob to display the next runway for the selected airport. 4. Continue turning the small FMS knob to select the desired runway. 5. To remove the flashing cursor, press the FMS knob.
SECTION 7 – NAVIGATION 7.4 INTERSECTION INFORMATION 7.5 NDB INFORMATION Select the Intersection Information Page 1. Turn the large FMS knob to select the WPT page group. 2. Turn the small FMS knob to select the second rectangular page icon. Figure 7-7 NDB Information Page Select the NDB Information Page 1. Turn the large FMS knob to select the WPT page group. 2.
SECTION 7 – NAVIGATION 7.6 VOR INFORMATION 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 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.
SECTION 7 – NAVIGATION Access Runway Information for the Selected Airport 2. Press the ENT key to display airport information. Press the ENT key again (cursor is on ‘BACK’) to return to the list. 1. Press the RNWY softkey located at the bottom of the display. 3. 2. Turn the small FMS knob to select the desired runway. Load an Airport COM Frequency into the Active COM 1. Turn the large FMS knob to place the cursor on the desired airport frequency shown in the window.
SECTION 7 – NAVIGATION 2. Turn the small FMS knob to select the second rectangular page icon. View Information on the Nearest Intersection 1. 2. Press the FMS knob to activate the cursor. Turn either FMS knob to select the desired intersection. Press the ENT key. 7.10 NEAREST NDB on the Nearest NDB Page pertains to the selected NDB. 7.11 NEAREST VOR Select the Nearest VOR Page 1. Turn the large FMS knob to select the NRST page group. 2.
SECTION 7 – NAVIGATION Select and Load a VOR Frequency 1. With the Nearest VOR Page selected, press the FREQ softkey to highlight the VOR frequency for the selected VOR. 2. Press the ENT key. The selected VOR frequency is placed in the NAV standby frequency field. OR Press the MENU key. Select the Select Frequency Window option and press the ENT key. Press the ENT key again when the frequency field is highlighted to place the selected VOR frequency in the NAV standby field.
SECTION 7 – NAVIGATION Select and Load the Nearest ARTCC, FSS, or Weather Frequency 1. With the Nearest Frequencies Page selected, press the ARTCC, FSS, or Wx softkey. 2. Turn the large FMS knob to select the frequency. 3. Press the ENT key to load the frequency into the ‘COM’ frequency standby field. 7.14 NEAREST AIRSPACES displayed. • If the aircraft is within two nautical miles of an airspace and the current course takes the aircraft inside, ‘Ahead < 2 nm’ is displayed.
SECTION 7 – NAVIGATION This page intentionally left blank.
SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING 3. Turn the large FMS knob to highlight the latitude/longitude field or the Reference Waypoints field, depending on how the waypoint is to be defined. 4. Turn the FMS knobs to enter the position coordinates or the radial and distance from the reference waypoint. 5. Press the ENT key to accept the new waypoint. 6. Press the FMS knob to remove the flashing cursor.
SECTION 8 – FLIGHT PLANNING Modify a User Waypoint 1. With the User Waypoint Information Page displayed, press the FMS knob to activate the cursor. 2. Turn the large FMS knob to move the cursor to the desired field and turn the small FMS knob to make changes. 3. Press the ENT key to accept the changes. 4. Press the FMS knob to remove the flashing cursor. Figure 8-3 Active Flight Plan Window on the PFD 8.3 1.
SECTION 8 – FLIGHT PLANNING 2. Press the ACT LEG softkey (using MFD only). OR 3. 4. Press the MENU key, select the ‘Activate Leg’ option from the page menu and press the ENT key. This step must be used when activating a leg from the PFD. With ‘Activate’ highlighted, press the ENT key. 8.6 INVERT ACTIVE FLIGHT PLAN 1. From the Active Flight Plan Page, press the MENU key to display the Page Menu. 2. Turn the large FMS knob to highlight ‘Invert Flight Plan’ and press the ENT key.
SECTION 8 – FLIGHT PLANNING Figure 8-10 Create FPL on MFD 3. Turn the small FMS knob to display the Waypoint Information Page. Turn the small FMS knob to enter the first character of the identifier of the departure waypoint. Turn the large FMS knob to move the cursor to the next character field. Repeat using the FMS knobs until the desired identifier has been entered. 1. Press the FPL key and press the small FMS knob to activate the cursor. 2.
SECTION 8 – FLIGHT PLANNING 8.11 REMOVE A DEPARTURE, ARRIVAL, OR APPROACH FROM A FLIGHT PLAN 1. 2. 3. With the Active or Stored Flight Plan Page displayed, press the small 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. 8.
SECTION 8 – FLIGHT PLANNING 3. 4. 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. 2. Press the MENU key to display the Flight Plan Catalog options. 3. Turn the large FMS knob to highlight ‘Delete Flight Plan’ and press the ENT key. With ‘OK’ highlighted, press the ENT key to invert the flight plan. 4. A ‘Delete flight plan?’ confirmation window is displayed.
SECTION 8 – FLIGHT PLANNING 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. Figure 8-16 Trip Planning Page 4. For Direct-to planning, press the WPTS softkey and verify that the ‘from’ 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 ‘to’ waypoint field.
SECTION 8 – FLIGHT PLANNING This page intentionally left blank.
SECTION 9 – PROCEDURES SECTION 9: PROCEDURES 9.1 ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1. With the Navigation Map Page displayed, press the FPL key. 2. Press the LD DP softkey. If a flight plan is active, the departure airport will be displayed as the default. A list of available departures is also displayed. 3. If no flight plan is active, use the FMS knobs to enter the identifier of the desired airport. Press the ENT key. 4.
SECTION 9 – PROCEDURES 6. A second window is displayed listing available transitions for the arrival. Turn either FMS knob to highlight the desired transition waypoint and press the ENT key. 9.2 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.
SECTION 9 – PROCEDURES Figure 9-7 Selecting an Approach Transition 7. Turn the large FMS knob to highlight ‘Activate?’ and press the ENT key to activate the approach. Selecting ‘Load?’ will add the procedure to the flight plan without immediately using it for navigation guidance. Activate An Approach in the Active Flight Plan 1. With the Navigation Map Page displayed, press the PROC key. 2. Turn the large FMS knob to highlight ‘ACTIVATE APPROACH’. 3. Press the ENT key.
SECTION 9 – PROCEDURES This page intentionally left blank.
SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.2 STORMSCOPE® (OPTIONAL) WARNING: Use of the Stormscope system for hazardous thunderstorm penetration is prohibited. Weather information on the G1000 MFD is approved for weather avoidance only. Refer to the WX-500 Pilot’s Guide for detailed operation. 10.1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1. 2. 3. With the Navigation Map Page displayed, press the MENU key to display the Navigation Map Page Menu.
SECTION 10 – HAZARD AVOIDANCE At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The presence of Stormscope lightning data is indicated by the annunciation ‘LTNG < 25 nm’ in the upper right corner. 2. Turn the small FMS knob until the Stormscope Page is selected. Figure 10-5 Lightning Display Range Annunciation To select ‘cell’ or ‘strike’ as the Stormscope lightning mode: 1. With the Weather Group selected, press the ENT key.
SECTION 10 – HAZARD AVOIDANCE keys are displayed. Press the 360 softkey to display a 360˚ viewing are or press the ARC softkey to display a 120˚ viewing area. Press the CLEAR softkey to remove all Stormscope lightning data from the display. 10.3 XM WEATHER (OPTIONAL) WARNING: Use of XM weather for hazardous weather penetration is not recommended. Weather information provided by XM Radio Service is approved only for weather avoidance, not penetration. 1. Press the MAP softkey. 2.
SECTION 10 – HAZARD AVOIDANCE 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 Data Link Page. 3. Press the available softkeys to select the desired XM weather product. 4. Press the LEGEND softkey to view the legends for the selected products. If necessary, turn either FMS knob to scroll through the list.
SECTION 10 – HAZARD AVOIDANCE CELL MOV – pressing the CELL MOV softkey shows storm cell movement by displaying an arrow. pointing in the direction of predicted movement. The display is updated every 12 minutes. SIG/AIR – 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.
SECTION 10 – HAZARD AVOIDANCE • • • • • Surface Analysis Freezing Levels Winds Aloft County Warnings Cyclone Warnings Echo Top (Cloud Top and Echo Top Mutually Exclusive) Figure 10-10 Weather Product Symbols The XM Information Page in the AUX Page Group will display the weather products available for the current subscription. A green box by the weather product means that it is available.
SECTION 10 – HAZARD AVOIDANCE 10.4 TRAFFIC INFORMATION SERVICE (TIS) Traffic Advisory, aircraft is 400’ above & Traffic out of Traffic Mode descending, moving in the direction of the line range NOTE: If the G1000 is configured to use the optional Skywatch Traffic Advisory System, TIS will not be available for use. NOTE: Traffic Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site. Displaying Traffic on the Traffic Map Page 1.
SECTION 10 – HAZARD AVOIDANCE 10.5 TERRAIN AND OBSTACLE PROXIMITY NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. Color RED YELLOW Displaying Terrain and Obstacles on the Terrain Proximity Page 1. Turn the large FMS knob to select the Map Page Group. 2. Turn the small FMS knob to select the last rectangular page icon. 3. If desired, press the VIEW softkey to access the ARC and 360 softkeys.
SECTION 11 – ABNORMAL OPERATION 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 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.
SECTION 12 – ANNUNCIATIONS & ALERTS SECTION 12: ANNUNCIATIONS AND ALERTS 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: • Annunciation Window: The Annunciation window displays abbreviated annunciation text. The Annunciation window is located to the right of the Altitude and Vertical Speed windows on the PFD display (or the MFD if system is in reversionary mode).
SECTION 12 – ANNUNCIATIONS & ALERTS 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in Diamond DA42 and DA42L aircraft, uses three alert levels. • 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 in Figure 12-2.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 AIRCRAFT ALERTS The following alerts are configured specifically for the Diamond DA42 aircraft. See the Airplane Flight Manual for information regarding pilot responses. WARNING Alerts Annunciation Window Text L / R ENG TEMP L / R OIL TEMP L / R OIL PRES L/R ENG FIRE L / R GBOX TEMP L / R ALTN AMPS L / R STARTER L / R FUEL TEMP DOOR OPEN AP TRIM FAIL Alerts Window Message Left/right engine coolant temp is >105 deg C.
SECTION 12 – ANNUNCIATIONS & ALERTS Annunciation Window Text DEICE LVL LO DEIC PRES HI DEIC PRES LO STICK LIMIT Alerts Window Message De-icing fluid level is low. De-icing pressure is high. De-icing pressure is low. Stick limiting system has failed. Audio Alert Single Aural Tone Annunciation Advisory Alerts Annunciation Window Text L / R GLOW ON L / R FUEL XFER Alerts Window Message Left/right engine glow plug active. Left/right fuel transfer from aux to main in progress.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.3 G1000 SYSTEM ANNUNCIATIONS Traffic Voice Alerts 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 Aircraft Flight Manual for additional information regarding pilot responses to these annunciations. The following voice alerts can be configured for ‘Male’ or ‘Female’ gender by using the Aux System Setup Page on the MFD.
SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment Display is not receiving altitude input from the air data computer. Display is not receiving vertical speed input from the air data computer. Display is not receiving valid heading input from AHRS. GPS information is either not present or is invalid for navigation use. Note that AHRS utilizes GPS inputs during normal operation. AHRS operation may be degraded if GPS signals are not present (see AFM).
SECTION 12 – ANNUNCIATIONS & 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.
SECTION 12 – ANNUNCIATIONS & ALERTS MFD & PFD Message Advisories Message DATA LOST – Pilot stored data was lost. Recheck settings. XTALK ERROR – A flight display crosstalk error has occurred. PFD1 SERVICE – PFD1 needs service. Return unit for repair. MFD1 SERVICE – MFD1 needs service. Return unit for repair. PFD1 CONFIG – PFD1 configuration error. Config service req’d. MFD1 CONFIG – MFD1 configuration error. Config service req’d. SW MISMATCH – GDU software mismatch. Xtalk is off.
SECTION 12 – ANNUNCIATIONS & ALERTS Database Message Advisories Alerts Window Message Comments MFD1 DB ERR – MFD1 aviation database error exists. The MFD and/or PFD detected a failure in the aviation database. Attempt to reload the aviation database. If problem persists, the G1000 system should be serviced. PFD1 DB ERR – PFD1 aviation database error exists. MFD1 DB ERR – MFD1 basemap database error exists. The MFD and/or PFD detected a failure in the basemap database.
SECTION 12 – ANNUNCIATIONS & ALERTS GMA 1347 Message Advisories Alerts Window Message GMA1 FAIL – GMA1 is inoperative. Comments 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. Config service req’d. The G1000 system should be serviced. MANIFEST – GMA1 software The audio panel has incorrect software installed.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories Alerts Window Message Comments GIA1 CONFIG – GIA1 configuration error. Config service req’d. The GIA1 and/or GIA2 configuration settings do not match backup configuration memory. The G1000 system should be serviced. GIA2 CONFIG – GIA2 configuration error. Config service req’d. GIA1 COOLING – GIA1 temperature too low. The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to warm up to operating temperature.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments COM1 RMT XFR – COM1 remote The COM1 and/or COM2 transfer switch is stuck in the enabled (or “pressed”) positransfer key is stuck. tion. Press the transfer switch again to cycle its operation. If the problem persists, COM2 RMT XFR – COM2 remote the G1000 system should be serviced. transfer key is stuck.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message G/S1 FAIL – G/S1 is inoperative. G/S2 FAIL – G/S2 is inoperative. G/S1 SERVICE – G/S1 needs service. Return unit for repair. G/S2 SERVICE – G/S2 needs service. Return unit for repair. Comments A failure has been detected in glideslope receiver 1 and/or receiver 2. The G1000 system should be serviced. A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver may still be available.
SECTION 12 – ANNUNCIATIONS & ALERTS GRS 77 Message Advisories Alerts Window Message AHRS TAS – AHRS not receiving airspeed. AHRS GPS – AHRS using backup GPS source. AHRS GPS – AHRS not receiving GPS information. AHRS GPS – AHRS not receiving backup GPS information. AHRS GPS – AHRS operating exclusively in no-GPS mode. MANIFEST – GRS1 software mismatch. Communication halted. BACKUP PATH – AHRS using backup data path. AHRS SERVICE – AHRS Magnetic-field model needs update.
SECTION 12 – ANNUNCIATIONS & ALERTS GDC 74A Message Advisories Alerts Window Message Comments 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 incorrect software installed. The G1000 system should be mismatch. Communication halted. serviced. BACKUP PATH – Airdata using backup The GDC 74A is using a backup communications data path.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Alerts Window Message Comments 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. WPT ARRIVAL – Arriving at waypoint Arriving at waypoint [xxxx], where [xxxx] is the waypoint name. -[xxxx] STEEP TURN – Steep turn ahead. A steep turn is 15 seconds ahead.
INDEX A B Abnormal COM operation 11-2 Activate a flight plan 8-2 Active flight plan 8-2 ADF 1-4 ADVISORY 12-1 Advisory alerts 12-4 Age 10-6 AHRS 12-14 Aircraft alerts 12-3 AIRMET 10-5 Airport frequency 7-6 Airport information 7-3 Airspace alerts 7-9 Airspeed indicator 2-3 Airspeed trend vector 2-3 Alerting System 12-1 Alerts 12-1 Alert levels 12-2 Altitude reference bug 2-4 Altitude trend vector 2-4 ALT knob 1-3 Annunciations 12-1 Approaches 9-2 Approach activation 4-4 Approach markers Signal augmentation 5
INDEX Messages 12-1 Message advisories 12-2, 12-8, 12-10, 12-12–12-16 METAR 10-3, 10-5 MFD 1-1, 4-4 Military interceptor operations code 4-5 MKR/MUTE 5-2 Mode selection softkeys 4-5 Morse code identifier 4-3 N Nav/Com controls 4-1 NAV1 5-2 NAV2 5-2 Navigation 7-1 Navigation status window 2-2 NAV Frequency Window 4-1 Nearest Airports Page 7-3, 7-5–7-9, 8-1 Nearest ARTCC & FSS frequencies 7-8 NEXRAD 10-3–10-6 O OBS 2-7 Operation 5-2 Optional NAV radios 4-3 Severe thunderstorm 10-5 SIGMET 10-5 Slip/Skid indi
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, SO51 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 © 2004, 2005 Garmin Ltd.
