Integrated Flight Deck Cockpit Reference Guide Diamond DA40/40F
Copyright © 2004-2006 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0369.11 or later for the Diamond DA40, DA40F. 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.
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: The Garmin G1000, as installed in the Diamond DA40 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.
WARNINGS, CAUTIONS, & NOTES 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.
RECORD OF REVISIONS Part Number 190-00324-00 Change Summary Initial Release 190-00324-01 Reformat of manual Added NAV/COM volume levels Added Flight Timer Added extended range fuel tanks Changed NAV1 and NAV2 on the PFD to VOR or LOC Moved altitude and airspeed trend vectors to opposite sides 190-00324-02 Added WX 500 Stormscope Added XM Weather Added ADF/DME Added bearing pointers Added fixed pitch propeller engine parameters Updated fixed pitch propeller engine parameters.
RECORD OF REVISIONS Blank Page RR-2 Garmin G1000 Cockpit Reference Guide for the DA40/40F
TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW.................................... 1-1 1.1 1.2 1.3 1.4 1.5 1.6 1.7 PFD/MFD Controls................................................... 1-2 PFD Softkeys............................................................ 1-4 MFD Softkeys .......................................................... 1-7 MFD Page Groups ................................................... 1-8 Backlighting .............................................................
TABLE OF CONTENTS Approach Mode (GPS, VAPP or LOC) .......................... 6-12 Go Around (GA) ........................................................ 6-12 6.7 Example Procedures Using AFCS ....................... 6-13 Departure ................................................................. 6-14 Intercepting a VOR Radial .......................................... 6-15 Flying a GPS Flight Plan............................................. 6-16 Flight Level Change (Descent)..............................
TABLE OF CONTENTS 8.7 Create a New Flight Plan ...................................... 8-3 Create a New Flight Plan Using the MFD ..................... 8-3 Create a New Flight Plan Using the PFD ...................... 8-4 8.8 Load a Departure ................................................... 8-4 8.9 Load an Arrival........................................................ 8-4 8.10 Load an Approach .................................................. 8-5 8.
TABLE OF CONTENTS 12.6 G1000 System Message Advisories .................. 12-8 MFD & PFD Message Advisories................................. 12-9 Database Message Advisories .................................. 12-10 GMA 1347 Message Advisories ............................... 12-11 GIA 63 Message Advisories ..................................... 12-11 GEA 71 Message Advisories .................................... 12-13 GTX 33 Message Advisories.....................................
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. Complete operating procedures for the complete system are found in the G1000 Pilot’s Guide (190-00592-02).
SECTION 1 SYSTEM OVERVIEW 1.
SECTION 1 SYSTEM OVERVIEW PFD and MFD controls function the same with the exception of the dedicated Automatic Flight Control System (AFCS) keys located only on the MFD bezel. (1) NAV VOL/ID Knob – Controls the NAV audio level. Press to turn the Morse code identifier ON and OFF. Volume level is shown in the field as a percentage. (2) NAV Frequency Transfer Key – Switches the standby and active NAV frequencies.
SECTION 1 SYSTEM OVERVIEW (16) ENT Key – Accepts a menu selection or data entry. This key is used to approve an operation or complete data entry. It is also used to confirm selections and information entries. (17) Dual ALT Knob – Sets the selected altitude in the box located above the Altimeter. The large knob selects the thousands, while the small knob selects the hundreds.
SECTION 1 SYSTEM OVERVIEW INSET OFF DCLTR TRAFFIC DCLTR-1 TOPO TERRAIN (optional) (optional) NEXRAD XM LTNG ALERTS BACK Press the BACK or OFF Softkey to return to the top level softkeys.
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. ALERTS – Press to display the Alerts Window. in the U.S.A., refer to ICAO standards for VFR codes in other countries). CODE – Press to display transponder code selection softkeys 0-7. 0 through 7 – Press numbers to enter code.
SECTION 1 SYSTEM OVERVIEW 1.3 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. ENGINE – Pressing this softkey makes available the LEAN and SYSTEM Softkeys which in turn access the Lean Display and the System Display, respectively.
SECTION 1 SYSTEM OVERVIEW 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. 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.
SECTION 1 SYSTEM OVERVIEW 6) Turn the large FMS Knob to highlight ‘MFD DSPL > AUTO’ and repeat steps 3 through 5. Figure 1-9 Database Update Prompt 3) Press the ENT Key to confirm the database updated. This prompt is displayed: Figure 1-8 PFD Setup Menu Window Figure 1-10 Database Update Confirmation 1.6 XM RADIO - AUTOMATIC MUTING XM Radio audio will be automatically muted when the aircraft groundspeed exceeds approximately 30 kts and the airspeed is less than approximately 80 kts.
SECTION 1 SYSTEM OVERVIEW These databases are not stored internally in the MFD or PFD. Supplemental Data Cards containing identical database versions must be kept in both displays to retain terrain and obstacle data. A Supplemental Data Card should be inserted into the bottom card slot of the PFD and MFD. NOTE: If the Supplemental Data Card is removed from the display, the TOPO and TERRAIN softkeys are not functional and are grayed out on the MFD Map Page.
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 Bo
SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICATOR Airspeed Trend Vector Actual Airspeed Vspeed References Speed Ranges (low end yellow band not displayed and other low end speed True Airspeed ranges differ on EASA Box certified aircraft) 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 Vspeed References are turned on or off in the Timer/References Window.
SECTION 2 FLIGHT INSTRUMENTS 2.3 ALTIMETER Altitude Alerting Altitude Reference Box Within 1000 ft Within 200 ft Deviation of ±200 ft Figure 2-8 Altitude Alerting Visual Annunciations Altitude Trend Vector Altitude Select Bug Current Altitude Visual annunciations appear in the Selected Altitude Box. Whenever the Selected Altitude is changed, the Altitude Alerter is reset. The Altitude Alerter is independent of the Automatic Flight Control System.
SECTION 2 FLIGHT INSTRUMENTS Within 2500 ft Within 100 ft 2.5 VERTICAL DEVIATION/GLIDESLOPE INDICATOR The Vertical Deviation/Glideslope Indicator appears when an ILS is tuned in the active NAV frequency field. Barometric Minimum Bug 2.6 VERTICAL SPEED INDICATOR Barometric Minimum Box Altitude Reached Selected Vertical Speed Vertical Speed Bug Vertical Speed Pointer Figure 2-9 Barometric Minimum Descent Altitude Alerting Visual Annunciations 2.
SECTION 2 FLIGHT INSTRUMENTS 14 Turn Rate Indicator and Heading Trend Vector 13 1 12 2 11 3 10 4 9 8 5 7 6 1 2 3 4 5 6 7 8 9 10 11 12 13 14 Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta turn rate trend vector shows the current turn rate. The end of the trend vector gives the heading predicted in six seconds, based on the present turn rate.
SECTION 2 FLIGHT INSTRUMENTS Course Deviation Indicator (CDI) Distance to Bearing Source 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 Pilot’s Guide for more details.
SECTION 2 FLIGHT INSTRUMENTS When using GPS as the navigation source, the following may appear: • INTEG – GPS information is either not present or is invalid for navigation use • WARN – GPS detects a position error • SUSP – Displayed when in OBS Mode indicating GPS waypoint sequencing is suspended. NOTE: The OBS Softkey is only displayed when navigating an active leg using GPS. .
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) SECTION 3: ENGINE INDICATION SYSTEM (EIS) 3.1 ENGINE DISPLAY RPM Gauge Fuel Flow Indicator In all cases green indicates normal operation, yellow indicates caution, and red indicates warning. Pressing the ENGINE Softkey makes available the LEAN and SYSTEM Softkeys which in turn provide access to the Lean Display and the System Display, respectively.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.2 LEAN ENGINE DISPLAY Cylinder Select The CYL SLCT Softkey can be utilized to obtain information about a particular cylinder. The CYL SLCT Softkey becomes disabled when a particular cylinder turns yellow or red, until the temperature decreases and returns to normal or when the ASSIST Softkey is pressed.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) 3.3 ENGINE SYSTEM DISPLAY If desired, use the DEC FUEL, INC FUEL and RST FUEL Softkeys 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.
SECTION 3 – ENGINE INDICATION SYSTEM (EIS) Blank Page 3-4 Garmin G1000 Cockpit Reference Guide for the DA40/40F
SECTION 4 – NAV/COM & TRANSPONDER SECTION 4: NAV/COM AND TRANSPONDER The NAV/COM controls and frequency boxes are located on the Primary Flight Display and the Multi Function Display in the same locations.
SECTION 4 – NAV/COM & TRANSPONDER Standby NAV Frequency Field Tuning Box Selected COM Frequency Selected NAV Frequency Active NAV Frequency Field Figure 4-2 Frequency Fields Frequency Transfer Arrow Active COM Frequency Field Tuning Box Figure 4-3 Frequency Transfer Arrow and Tuning Box NAV Controls COM Controls VOL/PUSH ID Knob VOL/PUSH SQ Knob Frequency Transfer Key Dual NAV Knob Dual COM Knob • Turn to tune in desired frequencies. • Press to change tuning box positions.
SECTION 4 – NAV/COM & TRANSPONDER 4.1 RADIO STATUS INDICATIONS • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception. • TX – When a COM radio is transmitting, a 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.
SECTION 4 – NAV/COM & TRANSPONDER 4.6 DME Radio (optional) FREQUENCY AUTO-TUNING Auto-tuning on the PFD Figure 4-8 ADF/DME Tuning Window Change the DME tuning source: 1) 2) From the tuning window, turn the large FMS Knob to highlight the desired DME source. Turn the small FMS Knob to display the selection window. Turn the FMS Knob to select the desired mode and press the ENT Key.
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 Blank Page 4-6 Garmin G1000 Cockpit Reference Guide for the DA40/40F
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 Outer Marker Annunciator Middle Marker Annunciator 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.
SECTION 5 – AUDIO PANEL 5.4 INTERCOM SYSTEM (ICS) ISOLATION Press the PILOT and/or COPLT Key to select who is isolated from hearing the NAV/COM radios and music. Selection scenarios are addressed in Table 5-1. 5.5 INTERCOM SQUELCH CONTROL Select manual squelch for intercom audio by pressing the MAN SQ Key to light the annunciator. Pressing the small VOL/SQ Knob now switches between volume and squelch adjustment by lighting VOL or SQ respectively.
SECTION 5 – AUDIO PANEL 5.6 DIGITAL CLEARANCE RECORDER AND PLAYER Each reception of primary active COM audio is automatically recorded in a memory block. When the next transmission is received, it is recorded in the next 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 also being active, ‘PTRM’ is displayed in the AFCS System Status Box on the PFD. Pressing the ARM switch also acknowledges an autopilot disconnect. The GFC 700 AFCS is optional on the DA40 and DA40F. In aircraft without the GFC 700 option, refer to the operating instructions for the installed autopilot system for details.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Active Mode Autopilot Status Armed Mode Roll Axis Modes Mode Reference Armed Mode Active Mode Pitch Axis Modes AFCS Status Box System Status Annuciation (see Annunciations & Alerts) Selected Altitude Box Aircraft Attitude Symbol Flight Director Command Bars Figure 6-3 PFD AFCS Display 6.2 OVERSPEED PROTECTION An overspeed annunciation (flashing inverse video) is displayed above the airspeed tape.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Automatic Disengagement 6.4 Automatic disengagement typically occurs due to a failure. Automatic disengagement is annunciated by a flashing ‘AP’, alternating red on white and white on red in the Autopilot Status Field. Also, the autopilot disconnect aural alert will be heard. Both the annunciation and the aural alert will continue until acknowledged by pressing the AP DISC button or the AP TRIM ARM switch.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Pitch Hold Mode (PIT) 1) Press the AP or FD Key. ‘PIT’ will be displayed in green in the Active Mode Field of the AFCS Status Box. The system will maintain or give command bar direction for a constant pitch attitude (pitch reference) depending on which key is pressed. selected altitude is reached ‘ALT’ will flash in green for 10 seconds in the Acitve Mode Field, after which the annunciation stops flashing.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Altitude Hold Mode (ALT) 3) 1) Press the ALT Key. The flight director is activated (if not already active) and ‘ALT’ is now displayed in green in the Active Mode Field with the current altitude displayed in the Altitude Reference Field. 2) Pitch commands will be given to manually maintain the current altitude. Press the AP Key to engage the autopilot for maintaining the current altitude.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Vertical Speed Mode (VS) 1) Press the VS Key. The flight director is now activated (if not already active) and ‘VS’ is displayed in green in the Active Mode Field and the Vertical Speed Bug will appear on the Vertical Speed Indicator. Pitch commands are given to manually maintain vertical speed. Press the AP Key to engage the autopilot for maintaining the current vertical speed.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flight Level Change Mode (FLC) 1) 2) 3) Select the desired altitude by turning the ALT Knob to set the altitude in the Altitude Select Box. This altitude must be selected first because Flight Level Change mode will only fly toward a selected altitude. Press the FLC Key. The flight director is activated (if not already active) and ‘FLC’ is now displayed in green in the Active Mode Field and the Airspeed Bug will appear on the Airspeed Indicator.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go Around Mode (GA) Glideslope (GS) Pressing the GA button (not located on the MFD) engages the flight director in a wings level, 7-degree pitchup attitude. Go Around mode disengages the autopilot, and arms Altitude Hold Mode automatically. Subsequent autopilot engagement is also allowed. If the pitch attitude is changed manually (e.g with the CWS button or the NOSE UP/NOSE DN Keys), Pitch and Roll Hold modes will automatically be selected.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.6 If the aircraft bank angle is < 6 degrees when the key is pressed, the aircraft will be maintained at wings level. If only the flight director is active, command bars give guidance to maintain wings level. ROLL AXIS MODES Mode annunciations for active roll axis modes are shown in green during normal operation.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Heading Select Mode (HDG) 1) 2) 3) Turn the HDG Knob to move the heading bug on the HSI to the desired heading. When the knob is turned, the Selected Heading Box will appear and remain for three seconds after the knob stops moving. The selected heading will be displayed in the Selected Heading Box. With the autopilot and/or flight director engaged, press the HDG Key. ‘HDG’ is now displayed in green in the Active Mode Field.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Navigation Mode (GPS, VOR, LOC, or BC) Pressing the NAV Key activates the Navigation Mode. The Navigation mode acquires and tracks the selected navigation receiver on the HSI (e.g. GPS, VOR or LOC). GPS roll steering commands are followed when the HSI is in GPS mode, and creates roll steering commands from the Selected Course and deviation when the HSI is in VOR, LOC, or BC (backcourse) modes.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Approach Mode (GPS, VAPP or LOC) The Approach mode acquires and tracks the selected navigation receiver on the HSI (GPS, VOR or LOC). This mode uses the selected navigation receiver deviation and desired course inputs to fly the approach. The Approach mode provides greater sensitivity for VOR tracking than Navigation mode, and allows the autopilot to fly an ILS approach with a glideslope.
SECTION 6 – AUTOMATIC FLIGHT CONTROL 6.7 EXAMPLE PROCEDURES USING AFCS NOTE: The diagrams in the following examples are for instructional purposes only and may not be used for navigation. This section provides a scenario-based set of procedures showing various autopilot modes used during a flight. In this scenario, the aircraft departs Reid-Hillview Airport (KRHV) from runway 13L, enroute to Fresno Yosemite International Airport (KFAT).
SECTION 6 – AUTOMATIC FLIGHT CONTROL Departure 3) Activate Heading Select Mode while the autopilot is engaged in the climb. Climb to the selected altitude and fly an assigned heading: a) Use the HDG Knob to set the Selected Heading to 070°. 1) Upon takeoff, set the Selected Altitude to 7000 feet using the ALT Knob. b) Press the HDG Key. The autopilot follows the Heading Bug on the HSI and turns the aircraft to the desired heading.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial NOTE: Changing the HSI mode cancels Navigation Mode and causes the flight director to revert to Roll Hold Mode. During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Airway V107 to Panoche VORTAC (PXN) should now be intercepted. 1) Tune the VOR frequency and activate Heading Select Mode. a) Use the CDI Softkey to set the HSI mode to VOR. c) Press the NAV Key to arm Navigation Mode.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flying a GPS Flight Plan 1) Enter Panoche VORTAC (PXN) and Clovis VORTAC (CZQ) into the GPS flight plan, in preparation to intercept this leg. 2) Transition from VOR to GPS Navigation Mode. a) Use the CDI Softkey to put the HSI in GPS mode. This cancels VOR mode on the HSI and the flight director loses the VOR signal. As a result, the VOR annunciation flashes yellow.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Flight Level Change (Descent) While flying the GPS leg from Panoche VORTAC to Clovis VORTAC, the aircraft is cleared to make a descent to 3000 feet in preparation for the approach to KFAT. 1) Enter Flight Level Change Mode. a) Using the ALT Knob, set the Selected Altitude to 3000 feet. b) Press the FLC Key to activate Flight Level Change Mode. The annunciation ‘FLC’ appears next to the Airspeed Reference, which defaults to the current aircraft airspeed, 142 knots.
SECTION 6 – AUTOMATIC FLIGHT CONTROL ILS Approach 3) In preparation for approach, tune the localizer frequency and select LOC mode on the HSI. 1) Transition from GPS Navigation Mode to Heading Select Mode. 4) Press the APR Key when cleared for approach to arm the Approach Mode. ‘LOC’ and ‘GS’ appear in the armed roll and pitch mode fields, respectively. The autopilot and flight director determine when to begin the turn to intercept the final approach course.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Go-Around / Missed Approach 4) To use the autopilot to fly the hold in Heading Select Mode, set the Selected Heading using the HDG Knob and press the HDG Key. Use the HDG Knob guide the aircraft for the remainder of the hold. 1) Push the GA button at the Decision Height and apply full power to execute a missed approach. The flight director Command Bars establish a nose-up climb to follow.
SECTION 6 – AUTOMATIC FLIGHT CONTROL Blank Page 6-20 Garmin G1000 Cockpit Reference Guide for the DA40/40F
SECTION 7 – NAVIGATION SECTION 7: NAVIGATION The following discussions pertain to the Multi Function Display, unless otherwise indicated. 7.1 NAVIGATION MAP PAGE Select the MAP Page Group 1) Turn the large FMS Knob until ‘MAP’ is highlighted in the Page Group Box in the lower right of the MFD display. 2) Turn the small FMS Knob to select the first MAP page (indicated by a solid rectangular icon).
SECTION 7 – NAVIGATION 3) Turn the small FMS Knob to display a list of waypoints or airports. 4) Continue turning the small FMS Knob to scroll through the list and highlight the desired waypoint or airport. 5) Press the ENT Key to confirm the selection. Press ENT again to activate a Direct-to. Re-center the CDI to the Destination Waypoint Press the Direct-to ( ) Key, followed by pressing the ENT Key twice. If a missed approach point (MAP) is the current destination, the approach will be canceled.
SECTION 7 – NAVIGATION 7.3 AIRPORT INFORMATION a list is displayed from which to choose the desired location. 6) To remove the flashing cursor, press the FMS Knob. Access Runway Information 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to place the cursor on the ‘RUNWAYS’ identifier field. 3) Turn the small FMS Knob to display the next runway for the selected airport.
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.
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 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.
SECTION 7 – NAVIGATION 7.9 NEAREST INTERSECTIONS 7.10 NEAREST NDB Figure 7-11 Nearest Intersections Page Select the Nearest Intersections Page 1) 2) Turn the large FMS Knob to select the ‘NRST’ page group. Turn the small FMS Knob to select the second rectangular page icon. 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.
SECTION 7 – NAVIGATION 7.11 NEAREST VOR 2) 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. 3) Press the ENT Key. The selected VOR frequency is placed in the NAV standby frequency field. Press the FMS Knob to remove the flashing cursor. 7.
SECTION 7 – NAVIGATION 3) Press the FMS Knob to remove the flashing cursor. 7.14 NEAREST AIRSPACES 7.13 NEAREST FREQUENCIES Figure 7-16 Nearest Airspaces Page Select the Nearest Airspaces Page Figure 7-15 Nearest Frequencies Page 1) Turn the large FMS Knob to select the ‘NRST’ page group. 2) Turn the small FMS Knob to select the seventh rectangular page icon. Select the Nearest Frequencies Page 1) Turn the large FMS Knob to select the ‘NRST’ page group.
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 place 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.
SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING 4) Repeat steps 2 and 3 until the desired name is entered. The following discussions pertain to the Multi Function Display, unless otherwise indicated. 5) Press the ENT Key. 6) Press the ENT Key a again to accept the new waypoint identifier. 7) The cursor is now in the ‘REFERENCE WAYPOINTS’ field. If desired, the waypoint can be defined by a reference waypoint.
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 captured position. 4) Turn the FMS Knobs to select a waypoint name.
SECTION 8 – FLIGHT PLANNING 8.4 ACTIVATE A FLIGHT PLAN LEG 1) From the Active Flight Plan Page, press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired destination waypoint. 2) Press the ACT LEG Softkey (using MFD only). 4) Figure 8-7 Delete Flight Plan Confirmation 8.6 OR 3) the flight plan. This will not delete the stored flight plan, only the active flight plan. Press the MENU Key, select the ‘Activate Leg’ option from the page menu and press the ENT Key.
SECTION 8 – FLIGHT PLANNING 2) Press the NEW Softkey to display a blank flight plan window for the first empty storage location. NOTE: After the first leg is entered (using the PFD only), it is immediately activated. 1) Press the FPL Key, then press the FMS Knob to activate the cursor. 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.
SECTION 8 – FLIGHT PLANNING 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 1) With the Active or Stored Flight Plan Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to highlight the title for the approach, departure or arrival to be deleted. Titles appear in white directly above the procedure’s waypoints.
SECTION 8 – FLIGHT PLANNING 8.15 INVERT AND ACTIVATE A STORED FLIGHT PLAN 1) From the Flight Plan Catalog Page, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to highlight the desired flight plan. 3) Press the INVERT Softkey. ‘Invert and activate stored flight plan?’ will be displayed. 4) 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.
SECTION 8 – FLIGHT PLANNING Starting WPT (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.
SECTION 8 – FLIGHT PLANNING 8.20 VERTICAL NAVIGATION (VNAV) PAGE 5) Press the ENT Key. The cursor is now positioned over the ‘Before’ and ‘After’ field. NOTE: An active flight plan or Direct-to must be entered in order to utilize VNAV. 6) Turn the small FMS Knob to select whether the previously set distance is ‘Before’ or ‘After’ the endpoint. NOTE: VNAV is advisory only and cannot be coupled to the autopilot. 7) Press the ENT Key. The cursor is now placed over the VNAV profile endpoint field.
SECTION 8 – FLIGHT PLANNING 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 profiled 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.
SECTION 8 – FLIGHT PLANNING Blank Page 8-10 Garmin G1000 Cockpit Reference Guide for the DA40/40F
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.
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. 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).
SECTION 9 – PROCEDURES 6) The cursor will move to the TRANSITIONS field. Turn the large FMS Knob to highlight the desired transition waypoint and press the ENT Key. (The “Vectors” option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course.) 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.
SECTION 9 – PROCEDURES Blank Page 9-4 Garmin G1000 Cockpit Reference Guide for the DA40/40F
SECTION 10 – HAZARD AVOIDANCE SECTION 10: HAZARD AVOIDANCE 10.2 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. 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.
SECTION 10 – HAZARD AVOIDANCE 3) Press the WX Softkey to display METAR and TAF text (METAR and TAF information is updated every 12 minutes). METAR Text TAF Text WX Softkey Figure 10-5 METAR and TAF Text Displayed on the Airport (Weather) Information Page Displaying Weather on the Weather Data Link Page Select the Weather Data Link Page: 10-2 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the fourth rectangular page icon.
SECTION 10 – HAZARD AVOIDANCE ECHO TOP – Press the ECHO TOP Softkey to show the location, elevation, and direction the highest radar echo. This may not indicate the top of a storm or clouds, only the highest radar return echo. 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.
SECTION 10 – HAZARD AVOIDANCE Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that displays the text of the report. Panning over an airport with METAR information does not 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.
SECTION 10 – HAZARD AVOIDANCE Weather Product SIGMETs/AIRMETs City Forecasts County Warnings Cyclone Warnings Echo Tops Freezing Levels METARs Lightning NEXRAD Radar Coverage Cell Movement Surface Analysis TFRs Winds Aloft TAFs Clouds Tops Expires After (minutes) 60 60 60 60 30 60 90 30 30 30 30 60 60 60 60 60 10.3 TRAFFIC INFORMATION SERVICE (TIS) NOTE: Traffic Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site.
SECTION 10 – HAZARD AVOIDANCE Traffic Advisory, aircraft is 400’ above & Traffic out of Traffic Mode descending, moving in the direction of the line range 10.4 TERRAIN AND OBSTACLE PROXIMITY NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. Displaying Terrain and Obstacles on the Terrain Proximity Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the last rectangular page icon.
SECTION 10 – HAZARD AVOIDANCE Color RED YELLOW Indication WARNING: Terrain/Obstacle at or within 100’ below or above aircraft altitude. CAUTION: Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. Displaying Terrain and Obstacles on the Navigation Map 1) With the Navigation Map displayed, press the MAP Softkey. 2) Press the TERRAIN Softkey. Terrain and obstacle proximity will now be displayed on the map.
SECTION 10 – HAZARD AVOIDANCE 10.5 TERRAIN AWARENESS & WARNING SYSTEM (TAWS) DISPLAY (OPTIONAL) NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south. NOTE: TAWS operation is only available when the G1000 is configured for a TAWS-B installation. Displaying Terrain on the TAWS Page 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the TAWS Page.
SECTION 10 – HAZARD AVOIDANCE Color Red Terrain/Obstacle Location Suggested Pilot Response Terrain/Obstacle at or within 100’ below or above aircraft altitude. Initiate climb and/or turn away from terrain/obstacle. Yellow Terrain/Obstacle between 100’ and 1000’ below current aircraft altitude. Be aware of surroundings. Be prepared to take action. Black Terrain/Obstacle is more than 1000’ below aircraft altitude. No action required.
SECTION 10 – HAZARD AVOIDANCE Manual System Test A system test is automatically performed at power-up. After sucessful completion of the test, “TAWS System Test, OK” will be heard. The system test may also be initiated manually, but only when the aircraft is on the ground. To manually verify proper operation of the aural and visual annunciations of the system, perform the following steps. 1) 2) 3) While the TAWS Page is displayed, press the MENU Key. Turn the small FMS Knob to select ‘Test TAWS’.
SECTION 10 – HAZARD AVOIDANCE to be closing (descending) upon terrain at an excessive speed. Figure 10-16 displays the correlation between height above terrain and descent rate, resulting in the two EDR alerts. EDR alerts have two levels of severity, caution (sink rate) and warning (pull-up). 5000 3500 The purpose of the aural alert message “Five-hundred” is to provide an advisory alert to the aircrew that the aircraft is five-hundred feet above terrain.
SECTION 10 – HAZARD AVOIDANCE Pop-up Alerts When the Navigation Map Page is displayed, and a terrain or obstacle alert is issued, a pop-up window is displayed with the appropriate alert. Figure 10-18 Alert Pop-Up Press the ENT Key to display the TAWS Page, or press the CLR Key to remain on the Navigation Map Page.
SECTION 10 – HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages.
SECTION 10 – HAZARD AVOIDANCE The following system status annunciations may also be issued. PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Availble” will be heard when sufficient GPS signal is re-established.
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 & ALERTS NOTE: The Airplane Flight Manual Supplement supersedes information found in this document. System Annunciation Red ‘X’ Annunciation Window Alerts Window Figure 12-1 G1000 Alerting System ALERTS Softkey Annunciation 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.
SECTION 12 – ANNUNCIATIONS & ALERTS • Audio Alerting System: The G1000 system issues audio alert tones when specific system conditions are met. See the Alert Levels Definitions section for more information. Figure 12-2 WARNING Softkey Annunciation 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in Diamond DA40 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.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.2 AIRCRAFT ALERTS The following alerts are configured specifically for the Diamond DA40 aircraft. See the Flight Manual Supplement for information regarding pilot responses. WARNING Alerts Annunciation Window Text OIL PRES LO FUEL PRES LO FUEL PRES HI ALTERNATOR STARTER ENGD DOOR OPEN TRIM FAIL Alerts Window Message Oil pressure is below 25 psi. Fuel pressure is below 14 psi. (1.0 psi on DA40F) Fuel pressure is greater than 35 psi. (8 psi on DA40F) Alternator failed.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.3 AFCS ALERTS System Status Annunciation System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD. Figure 12-5 AFCS System Status Annunciation Condition Pitch Failure Roll Failure Roll axis control failure. AP is inoperative. AP TRIM Switch Stuck, or Pitch Trim Axis Control Failure System Failure If annunciated when AP is engaged, a failure has occurred in the pitch trim system.
SECTION 12 – ANNUNCIATIONS & ALERTS 12.4 TAWS ALERTS Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD.
SECTION 12 – ANNUNCIATIONS & ALERTS TAWS System Status Annunciations PFD/MFD TAWS Page Annunciation MFD Pop-Up Alert Aural Message TAWS System Test Fail None “TAWS System Failure” TAWS Alerting is disabled None None No GPS position or excessively degraded GPS signal None “TAWS Not Available” “TAWS Availble” will be heard when sufficient GPS signal is re-established. System Test in progress None None None “TAWS System Test OK” Alert Type None System Test pass 12.
SECTION 12 – ANNUNCIATIONS & ALERTS System Annunciation Comment Display system is not receiving airspeed input from air data computer. 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.
SECTION 12 – ANNUNCIATIONS & ALERTS A red ‘X’ may be the result of an LRU or an LRU function failure. The Figure 12-6 illustrates all possible flags and the responsible LRUs.
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 Database Message Advisories (Cont.) Alerts Window Message DB MISMATCH – Airport Terrain database mismatch. Xtalk is off Comments The PFD and MFD have different airport terrrain databases installed. Crossfill is off. Install correct airport terrain database in both displays. 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.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments GIA1 SERVICE – GIA1 needs service. Return the unit for repair. The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000 system should be serviced. GIA2 SERVICE – GIA2 needs service. Return the unit for repair. There is a hardware mismatch between GIA1 and GIA2. The G1000 system should HW MISMATCH – GIA hardware be serviced. mismatch. Communication halted.
SECTION 12 – ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments DGRD GPS ACC – GPS position GPS position accuracy has been degraded and RAIM is not available. accuracy degraded & RAIM unavailable. GPS1 FAIL – GPS1 is inoperative. A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver is unavailable. The G1000 system should be serviced. GPS2 FAIL – GPS2 is inoperative. GPS1 SERVICE – GPS1 needs service. Return unit for repair.
SECTION 12 – ANNUNCIATIONS & ALERTS GTX 33 Message Advisories Alerts Window Message XPDR1 CONFIG – XPDR1 config error. Config service req’d. MANIFEST – GTX1 software mismatch. Communication halted. BACKUP PATH – XPDR1 using backup data path. Comments The transponder configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. The transponder has incorrect software installed. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS GMU 44 Message Advisories Alerts Window Message HDG FAULT – AHRS1 magnetometer fault has occurred. MANIFEST – GMU1 software mismatch. Communication halted. Comments A fault has occurred in the GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The G1000 system should be serviced. The GMU 44 has incorrect software installed. The G1000 system should be serviced.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Alerts Window Message FPL WPT MOVE – Flight plan waypoint moved. TIMER EXPIRD – Timer has expired. DB CHANGE – Database changed. Verify user modified procedures. FPL TRUNC – Flight plan has been truncated. APPR VPROF – Approaching VNAV profile. APPR TRG ALT – Approaching target altitude. LOCKED FPL – Cannot navigate locked flight plan. WPT ARRIVAL – Arriving at waypoint -[xxxx] STEEP TURN – Steep turn ahead.
SECTION 12 – ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Alerts Window Message SLCT AUTOSEQ – Select auto sequence mode. SLCT FREQ – Select appropriate frequency for approach. SLCT NAV – Select NAV on CDI for approach. NO WGS84 WPT – Non WGS 84 waypoint for navigation -[xxxx] TRAFFIC FAIL – Traffic device has failed. Comments The system notifies the pilot to select auto-sequence mode. Press the OBS Softkey to deactivate the OBS mode.
SECTION 12 – ANNUNCIATIONS & ALERTS Blank Page 12-18 Garmin G1000 Cockpit Reference Guide for the DA40/40F
INDEX A Abnormal COM operation 11-2 Activate a flight plan 8-3 Active flight plan 8-2 ADF 1-5, 4-3 ADVISORY 12-1 Advisory alerts 12-3 AFCS 1-3, 6-1 – 6-4, 6-6, 6-7, 6-9, 6-11, 6-12, 6-13, 12-4 Age 10-4 AHRS 12-14 Aircraft alerts 12-3 AIRMET 10-3 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 Pop-Up 10-12 Altitude Hold 1-4 Altitude hold 1-4, 6-3 – 6-8, 6-10 Altitude trend vector 2-4 ALT
INDEX HSI 2-5 Hurricanes 10-3 Military interceptor operations code 4-5 Missed Approach 6-19 Mistrim 12-4 MKR/MUTE 5-2, 5-4 Mode selection softkeys 4-5 Morse code identifier 4-3 I ICAO 4-5 ID 4-3 IDENT function 4-5 Imminent Terrain Impact 10-10 Impact point 10-10 INC FUEL 3-3 Inhibit 10-9 Inhibit TAWS 10-9 INTEG 2-8 Interrogations 4-5 IOI 10-10, 10-13, 12-5 ITI 10-10 N K Key(s) 1-4 L Lean engine 3-2 Lighted obstacle 10-11 Load approach 8-5 Load a VOR frequency 7-8 Load departure 8-4 Load the frequency fo
INDEX Tropical storms 10-3 TX 4-3 U Unlighted obstacle 10-11 V Vertical Deviation/Glideslope indicator 2-5 Vertical navigation profile 8-8 Vertical speed 1-4, 2-5, 6-3, 6-6 Vertical Speed Bug 2-5 Vertical Speed Mode 6-6 VFR code 4-5 VHF 4-1 VOL/PUSH ID 4-2 VOL/PUSH SQ 4-2, 4-3 Volume/squelch 5-3 VS 1-4, 6-3, 6-6 Vspeeds 2-3 W WARN 2-8 Warning 12-1, 12-2 Weather data link page 10-2 Weather product symbol 10-4 Weather product symbols 10-4 Weather warnings 10-3 Wind direction 10-3 Wind speed 10-3 X XPDR Sof
INDEX Blank Page.
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