Manuale d’uso / di manutenzione del prodotto DA40F del fabbricante Garmin
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Integr ated Flight Deck Cockpit Refer ence Guide Diamond DA40/40F.
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Garmin G1000 Cockpit Reference Guide for the D A40/40F Copyright © 2004-2006 Garmin Ltd. or its subsidiaries . All rights reserved. T his manual reflects the operation of System Software version 0369.
Garmin G1000 Cockpit Reference Guide for the D A40/40F W ARNINGS, CAUTIONS, & NOTES W ARNING: Navigation and terrain separation must NO T be predicated upon the use of the terrain function.
Garmin G1000 Cockpit Reference Guide for the D A40/40F W ARNINGS, CAUTIONS, & NOTES W ARNING: T he Garmin G1000, as installed in the Diamond DA40 aircraft, has a very high degree of functional integrity .
Garmin G1000 Cockpit Reference Guide for the D A40/40F W ARNINGS, CAUTIONS, & NOTES NO TE: 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.
Garmin G1000 Cockpit Reference Guide for the D A40/40F RECORD OF REVISIONS RR-1 Part Number Change Summary 190-00324-00 Initial Release 190-00324-01 Reformat of manual Added NA V/COM volume levels Add.
Garmin G1000 Cockpit Reference Guide for the D A40/40F RECORD OF REVISIONS RR-2 Blank P age.
Garmin G1000 Cockpit Reference Guide for the D A40/40F i T ABLE OF CONTENTS SECTION 1: SYSTEM OVER VIEW .................................... 1-1 1.1 PFD/MFD Controls ................................................... 1-2 1.2 PFD Softkeys ............
Garmin G1000 Cockpit Reference Guide for the D A40/40F ii T ABLE OF CONTENTS Approach Mode (GPS , V APP or LOC) .......................... 6-12 Go Around (GA) ........................................................ 6-12 6.7 Example Procedur es Using AFCS .
Garmin G1000 Cockpit Reference Guide for the D A40/40F iii T ABLE 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 .
Garmin G1000 Cockpit Reference Guide for the D A40/40F iv T ABLE OF CONTENTS 12.6 G1000 System Message Advisories .................. 12-8 MFD & PFD Message Advisories ................................. 12-9 Database Message Advisories .............
Garmin G1000 Cockpit Reference Guide for the D A40/40F 1-1 SECTION 1 SYSTEM OVERVIEW 1-1 SECTION 1: SYSTEM O VERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resour ce with which to find operating instructions on the major features of the G1000 system more easily .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 1-2 SECTION 1 SYSTEM OVERVIEW 1.1 PFD/MFD CONTROLS Figure 1-1 PFD/MFD Controls 4 2 1 6 5 7 9 8 3 12 13 11 10 16 15 14 MFD Only (with optional GFC.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 1-3 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) NA V VOL/ID Knob – Controls the NA V audio level.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 1-4 SECTION 1 SYSTEM OVERVIEW (16) ENT Key – Accepts a menu selection or data entry . This key is used to approve an operation or complete data entry . It is also used to confirm selections and information entries.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 1-5 SECTION 1 SYSTEM OVERVIEW INSET OFF TOPO TRAFFIC TERRAIN DCL TR DCL TR-2 DCL TR-3 DCL TR-1 NEXRAD Press the BACK or OFF Softkey to return to the top level softkeys.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 1-6 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.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 1-7 SECTION 1 SYSTEM OVERVIEW IDENT – Press to pr ovide special air craft position identification to Air T raffic Control (A TC). TMR/REF – Press to display the T imer/References W indow . NRST – Press to display the Near est Airports W indow .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 1-8 SECTION 1 SYSTEM OVERVIEW TRAFFIC – Pressing this softkey displays/ removes T raffic on the Navigation Map. TOPO – Pressing this softkey displays or removes topographic information on the Navigation Map.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 1-9 SECTION 1 SYSTEM OVERVIEW 6) T urn the large FMS Knob to highlight ‘MFD DSPL > A UT O’ and repeat steps 3 through 5.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 1-10 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.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 2-1 SECTION 2 FLIGHT INSTRUMENTS SECTION 2: FLIGHT INSTRUMENTS The following discussions pertain to the Primar y Flight Display , unless other wise indicated.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 2-2 SECTION 2 FLIGHT INSTRUMENTS Figure 2-2 Additional PFD Information 4 7 8 9 1 3 6 2 1 1 T raffic Annunciation 2 4 3 1 8 9 Inset Map Selected .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 2-3 SECTION 2 FLIGHT INSTRUMENTS 2.1 AIRSPEED INDICA TOR Figure 2-4 Airspeed Indicator Actual Airspeed Airspeed T rend V ector T r ue Airspeed Bo.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 2-4 SECTION 2 FLIGHT INSTRUMENTS 2.3 AL TIMETER Altitude Refer ence Box Altitude T rend V ector Curr ent Altitude Bar ometric Setting Box Figure .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 2-5 SECTION 2 FLIGHT INSTRUMENTS Within 100 ft Altitude Reached Within 2500 ft Figure 2-9 Barometric Minimum Descent Altitude Alerting Visual Annunciations Bar ometric Minimum Box Bar ometric Mini- mum Bug 2.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 2-6 SECTION 2 FLIGHT INSTRUMENTS Figure 2-12 Horizontal Situation Indicator (360º) 8 14 9 6 5 4 3 2 1 7 13 12 1 1 10 Heading Bug 2 3 6 4 5 7 1 T.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 2-7 SECTION 2 FLIGHT INSTRUMENTS 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.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 2-8 SECTION 2 FLIGHT INSTRUMENTS When using GPS as the navigation source, the following may appear: • INTEG – GPS information is either not p.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 3 – ENGINE INDICA TION SYSTEM (EIS) 3-1 SECTION 3: ENGINE INDICA TION SY STEM (EIS) 3.1 ENGINE DISPLA Y In all cases green indicates normal operation, yellow indicates caution, and red indicates warning.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 3 – ENGINE INDICA TION SYSTEM (EIS) 3-2 3.2 LEAN ENGINE DISPLA Y Cylinder Select The CYL SLCT Softkey can be utilized to obtain information about a particular cylinder .
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 3 – ENGINE INDICA TION SYSTEM (EIS) 3-3 3.3 ENGINE SY STEM DISPLA Y If desired, use the DEC FUEL, INC FUEL and RST FUEL Softkeys to adjust the amount of fuel remaining for totalizer calculations.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 3 – ENGINE INDICA TION SYSTEM (EIS) 3-4 Blank P age.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 4-1 SECTION 4 – NA V/COM & TRANSPONDER SECTION 4: NA V/COM AND TRANSPONDER The NA V/COM controls and frequency boxes are located on the Primary Flight Display and the Multi Function Display in the same locations.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 4-2 SECTION 4 – NA V/COM & TRANSPONDER Standby NA V Fr equency Field Active NA V Fr equency Field Active COM Fr equency Field Standby COM F.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 4-3 SECTION 4 – NA V/COM & TRANSPONDER 4.1 RADIO ST A TUS INDICA TIONS • RX – When a COM signal is received, a white ‘RX’ appears by the active COM frequency during signal reception.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 4-4 SECTION 4 – NA V/COM & TRANSPONDER DME Radio (optional) Figure 4-8 ADF/DME T uning Window Change the DME tuning source: 1) F rom the tuning window , turn the large FMS Knob to highlight the desired DME source .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 4-5 SECTION 4 – NA V/COM & TRANSPONDER 4.7 TRANSPONDER Mode Selection The STBY , ON and AL T Softkeys can be accessed by pressing the XPDR Softkey . Ground Mode (Automatic) GND is displayed when the aircraft is on the gr ound.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 4-6 SECTION 4 – NA V/COM & TRANSPONDER Blank P age.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 5-1 SECTION 5 – AUDIO P ANEL SECTION 5: AUDIO P ANEL T ransmitters (COM3 MIC is unavailable) T ransceiver Audio (COM 3 is unavailable) Split CO.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 5-2 SECTION 5 – AUDIO P ANEL 5.1 COM RADIO SELECTION Pressing the COM1 MIC or COM2 MIC Key selects the active transmitter (i.e., microphone). The associated receiver audio ( COM1 or COM2 ) also becomes selected when the COM MIC Key is pressed.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 5-3 SECTION 5 – AUDIO P ANEL 5.4 INTERCOM SY STEM (ICS) ISOLA TION Press the PILOT and/or COPL T Key to select who is isolated from hearing the NA V/COM radios and music. Selection scenarios are addressed in T able 5-1.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 5-4 SECTION 5 – AUDIO P ANEL 5.6 DIGIT AL CLEARANCE RECORDER AND PLA YER Each reception of primar y active COM audio is automatically recor ded in a memory block. When the next transmission is received, it is recor ded in the next memory block, and so on.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-1 SECTION 6: AUT OMA TIC FLIGHT CONTROL 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.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-2 Figure 6-3 PFD AFCS Display Armed Mode Active Mode Autopilot Status Mode Refer ence Active Mode Armed.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-3 Automatic Disengagement Automatic disengagement typically occurs due to a failure. Automatic disengagement is annunciated by a flashing ‘AP’, alter nating r ed on white and white on r ed in the Autopilot Status Field.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-4 Pitch Hold Mode (PIT) 1) Press the AP or FD K ey . ‘PIT’ will be displayed in green in the Active Mode Field of the AFCS Status Box.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-5 Altitude Hold Mode (AL T) 1) P res s the AL T K ey .
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-6 V ertical Speed Mode (VS) 1) Press the VS K ey . T he flight director is now activated (if not already active) and ‘VS’ is displayed in green in the Active Mode Field and the V ertical Speed Bug will appear on the V ertical Speed Indicator .
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-7 Flight Level Change Mode (FLC) 1 ) Select the desired altitude by turning the AL T 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 .
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-8 Go Around Mode (GA) Pressing the GA button (not located on the MFD) engages the flight director in a wings level, 7-degree pitch- up attitude. Go Around mode disengages the autopilot, and arms Altitude Hold Mode automatically .
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-9 6.6 ROLL AXIS MODES Mode annunciations for active r oll axis modes are shown in green during normal operation.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-10 Heading Select Mode (HDG) 1) T urn 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.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-11 Navigation Mode (GPS , VOR, LOC, or BC) Pressing the NA V Key activates the Navigation Mode. The Navigation mode acquires and tracks the selected navigation receiver on the HSI (e.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-12 Approach Mode (GPS , V APP or LOC) The Appr oach 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 appr oach.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-13 6.7 EXAMPLE PROCEDURES USING AFCS This section provides a scenario-based set of procedur es showing various autopilot modes used during a flight.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-14 Departure Climb to the selected altitude and fly an assigned heading: 1) Upon tak eoff , set the Selected Altitude to 7000 feet using the AL T Knob .
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-15 Intercepting a VOR Radial N OT E : 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.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-16 Flying a GPS Flight Plan 1) E nter P ano che VOR T AC (PXN) and Clo vis VOR T AC (CZQ) into the GPS flight plan, in prepar ation to intercept this leg.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-17 Flight Level Change (Descent) While flying the GPS leg from Panoche VOR T AC to Clovis VOR T AC, the aircraft is cleared to make a descent to 3000 feet in preparation for the appr oach to KF A T .
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-18 ILS Approach 1) T ra nsit ion from GPS Naviga tion Mode to Headin g Select Mode . a) Load the Runw ay 29R ILS approach for KF A T into the Flight Plan.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-19 Go-Around / Missed Approach 1) Push the GA button at the Decision Height and apply full power to execute a missed approach. T he flight director Command Bars establish a nose-up climb to follow .
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-20 Blank P age.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 7 – NA VIGA TION 7-1 SECTION 7: NA VIGA TION The following discussions pertain to the Multi Function Display , unless other wise indicated.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 7 – NA VIGA TION 7-2 3) T urn 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.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 7 – NA VIGA TION 7-3 7.3 AIRPORT INFORMA TION Figure 7-5 Airport Information P age Select the Airport Information Page 1) T urn the large FMS Knob to select the ‘WPT’ page group . 2) T urn the small FMS Knob to select the first rectangular page icon.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 7 – NA VIGA TION 7-4 7.4 INTERSECTION INFORMA TION Select the Intersection Information P age 1) T urn the large FMS Knob to select the ‘WPT’ page group . 2) T urn the small FMS Knob to select the second rectangular page icon.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 7 – NA VIGA TION 7-5 7.6 V OR INFORMA TION Figure 7-8 VOR Information P age Select the VOR Information P age 1) T urn the large FMS Knob to select the ‘WPT’ page group . 2) T urn the small FMS Knob to select the fourth rectangular page icon.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 7 – NA VIGA TION 7-6 3) Press the FMS Knob to remove the flashing cursor . Access Runway Information for the Selected Airport 1) With the Near est Airpo rts P age displ ayed , press the RNWY Softk ey to place the cursor in the ‘RUNW A Y S’ field.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 7 – NA VIGA TION 7-7 7.9 NEAREST INTERSECTIONS Figure 7-11 Nearest Inter sections P age Select the Nearest Inter sections P age 1) T urn the large FMS Knob to select the ‘NRST’ page group .
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 7 – NA VIGA TION 7-8 7.11 NEAREST VOR Select the Nearest VOR Page 1) T urn the large FMS Knob to select the ‘NRST’ page group . 2) T urn the small FMS Knob to select the fourth rectangular page icon.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 7 – NA VIGA TION 7-9 3) Press the FMS Knob to remove the flashing cursor . 7.13 NEAREST FREQUENCIES Figure 7-15 Nearest Fr equencies P age Select the Nearest Fr equencies Page 1) T urn the large FMS Knob to select the ‘NRST’ page group .
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 7 – NA VIGA TION 7-10 View Additional Details for a Listed Airspace 1) With the Nearest Airspace P age displayed, press the FMS Knob to activate the cursor . 2) T urn the large FMS Knob to scroll through the list, highlighting the desired airspace.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 8-1 SECTION 8 – FLIGHT PLANNING SECTION 8: FLIGHT PLANNING The following discussions pertain to the Multi Function Display , unless other wise indicated.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 8-2 SECTION 8 – FLIGHT PLANNING Create User Waypoints fr om the Navigation Map Page 1) With the Navig ation Map P age displ ayed, push the Joystick to activ ate the panning function. T he map pointer is displayed at the present aircraft position.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 8-3 SECTION 8 – FLIGHT PLANNING 8.4 ACTIV A TE A FLIGHT PLAN LEG 1) F rom the Active Flight Plan P age , press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired destination waypoint.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 8-4 SECTION 8 – FLIGHT PLANNING 2 ) Press the NEW Softk ey to display a blank flight plan window for the first empty storage location. Figure 8-10 Create FPL on MFD 3 ) T urn the small F M S Knob to display the W aypoint Information Window .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 8-5 SECTION 8 – FLIGHT PLANNING 8.10 LO AD AN APPROA CH See the Pr ocedures section for a discussion on loading and activating approach pr ocedures.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 8-6 SECTION 8 – FLIGHT PLANNING 8.15 INVERT AND ACTIV A TE A ST ORED FLIGHT PLAN 1) F rom the Flight Plan Catalog P age , press the FMS Knob to activate the cursor . 2 ) T urn the large F MS Knob to highlight the desired flight plan.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 8-7 SECTION 8 – FLIGHT PLANNING Figure 8-15 T rip Planning P age Starting WPT Ending WPT 4) F or Dire ct- to pla nni ng , pr ess t he WPT S Softk ey and verify that the starting w aypoint field in di ca tes ‘P .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 8-8 SECTION 8 – FLIGHT PLANNING 8.20 VERTICAL NA VIGA TION (VNA V) P AGE NO TE : An active flight plan or Direct-to must be entered in order to utilize VNA V . NO TE : VNA V is advisory only and cannot be coupled to the autopilot.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 8-9 SECTION 8 – FLIGHT PLANNING the target altitude. If the selected altitude is above the current aircr aft altitude , a profiled climb is created. If the selected altitude is below the current aircraft altitude , a profiled descent will be created.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 8-10 SECTION 8 – FLIGHT PLANNING Blank P age.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 9-1 SECTION 9 – PROCEDURES SECTION 9: PROCEDURES 9.1 ARRIV ALS AND DEP ARTURES Load and Activate a Departure Pr ocedure 1) With the Navi gat ion Map P age displa yed , pre ss the FPL K ey . 2) Pres s the LD DP Softk ey .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 9-2 SECTION 9 – PROCEDURES 6) A second window is displayed listing available tr ans itio ns for the arri va l. T urn eithe r FMS Knob to high lig ht the desi red tr ans iti on wa ypo int and press the ENT K ey .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 9-3 SECTION 9 – PROCEDURES 6) T he cursor will move to the TRANSITIONS field. T urn the large FMS Knob to highlight the desired transition waypoint and press the ENT K ey .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 9-4 SECTION 9 – PROCEDURES Blank P age.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-1 SECTION 10 – HAZARD A VOIDANCE SECTION 10: HAZARD A VOID ANCE 10.1 CUST OMIZING THE HAZARD DISPLA YS ON THE NA VIGA TION MAP 1) With the Navi gat ion Map P age displa yed , pre ss the MENU Key to display the Navigation Map P age Menu.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-2 SECTION 10 – HAZARD A VOIDANCE 3) Press the WX Softk ey to display MET AR and T AF text (MET AR and T AF information is updated every 12 minutes).
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-3 SECTION 10 – HAZARD A VOIDANCE 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 r eturn echo.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-4 SECTION 10 – HAZARD A VOIDANCE Note that pressing the ENT K ey when panning over an AIRMET or a SIGMET displays an information box that displays the text of the report.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-5 SECTION 10 – HAZARD A VOIDANCE W eather Product Expires After (minutes) SIGMETs/AIRMETs 60 City F orecasts 60 County W arnings 60 Cyclone .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-6 SECTION 10 – HAZARD A VOIDANCE T raffic out of range T raffic 1600’ above & climbing, moving in the dir ection of the line T raf.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-7 SECTION 10 – HAZARD A VOIDANCE Color Indication RED WARNING: T errain/Obstacle at or within 100’ below or above aircraft altitude . YELLOW CA UTION: T errain/Obstacle between 100’ and 1000’ below current aircraft altitude .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-8 SECTION 10 – HAZARD A VOIDANCE 10.5 TERRAIN AW ARENESS & W ARNING SY STEM (T AWS) DISPLA Y (OPTIONAL) NO TE: T errain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-9 SECTION 10 – HAZARD A VOIDANCE Color T errain/Obstacle Location Suggested Pilot Response Red T errain/Obstacle at or within 100’ below or above aircraft altitude . Initiate climb and/or turn away from terrain/obstacle .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-10 SECTION 10 – HAZARD A VOIDANCE Manual System T est A syst em tes t is aut oma ti cal ly perf or med at powe r -up. After sucessful completion of the test, “ T A WS System T est, OK ” will be heard.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-11 SECTION 10 – HAZARD A VOIDANCE 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.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-12 SECTION 10 – HAZARD A VOIDANCE 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.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-13 SECTION 10 – HAZARD A VOIDANCE T AWS Alerts Summary The following table shows the possible T A WS alert types with corresponding annunciations and aural messages.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 10-14 SECTION 10 – HAZARD A VOIDANCE The following system status annunciations may also be issued.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 11 – ABNORMAL OPERA TION 11-1 SECTION 11: ABNORMAL OPERA TION 11.1 REVERSIONAR Y MODE Should a system detected failure occur in either display , the G1000 automatically enters reversionary mode.
Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 11 – ABNORMAL OPERA TION 11-2 11.2 ABNORMAL COM OPERA TION When a COM tuning failure is detected by the system, the emer gency frequency (121.500 MHz) is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-1 SECTION 12 – ANNUNCIA TIONS & ALERTS SECTION 12: ANNUNCIA TIONS & ALERTS NO TE: T he Airplane Flight Manual Supplement supersedes information found in this document.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-2 SECTION 12 – ANNUNCIA TIONS & 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.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-3 SECTION 12 – ANNUNCIA TIONS & ALERTS 12.2 AIRCRAFT ALERTS The following alerts are configured specifically for the Diamond DA40 air craft. See the Flight Manual Supplement for information regar ding pilot responses.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-4 SECTION 12 – ANNUNCIA TIONS & ALERTS 12.3 AFCS ALERTS System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD. Condition Annunciation Description Pitch F ailure Pitch axis control failure .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-5 SECTION 12 – ANNUNCIA TIONS & ALERTS 12.4 T AWS ALERTS Annunciations appear on the PFD and MFD.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-6 SECTION 12 – ANNUNCIA TIONS & ALERTS T AWS System Status Annunciations Alert T ype PFD/MFD T A WS P age Annunciation MFD P op-Up Alert.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-7 SECTION 12 – ANNUNCIA TIONS & 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 .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-8 SECTION 12 – ANNUNCIA TIONS & ALERTS A r ed ‘X’ may be the result of an LRU or an LRU function failure.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-9 SECTION 12 – ANNUNCIA TIONS & ALERTS MFD & PFD Message Advisories Message Comments D A T A LOST – Pilot stored data was lost. Recheck settings. T he pilot profile data was lost. System reverts to default pilot profile and settings.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-10 SECTION 12 – ANNUNCIA TIONS & ALERTS Database Message Advisories Alerts Window Message Comments MFD1 DB ERR – MFD1 aviation database error exists . T he MFD and/or PFD detected a failure in the aviation database.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-11 SECTION 12 – ANNUNCIA TIONS & ALERTS Database Message Advisories (Cont.) Alerts Window Message Comments DB MISMA TCH – Airport T errain database mismatch. Xtalk is off T he PFD and MFD have different airport terrrain databases installed.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-12 SECTION 12 – ANNUNCIA TIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments GIA1 SER VICE – GIA1 needs service . Return the unit for repair . T he GIA1 and/or GIA2 self-test has detected a problem in the unit.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-13 SECTION 12 – ANNUNCIA TIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments DGRD GPS A CC – GPS position accuracy degr aded & RAIM unavailable . GPS position accuracy has been degr aded and RAIM is not available .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-14 SECTION 12 – ANNUNCIA TIONS & ALERTS GTX 33 Message Advisories Alerts Window Message Comments XPDR1 CONFIG – XPDR1 config error . Config service req’ d. T he transponder configuration settings do not match those of backup configur ation memory .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-15 SECTION 12 – ANNUNCIA TIONS & ALERTS GMU 44 Message Advisories Alerts Window Message Comments HDG F AUL T – AHRS1 magnetometer fault has occurred. A fault has occurred in the GMU 44.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-16 SECTION 12 – ANNUNCIA TIONS & ALERTS Miscellaneous Message Advisories (Cont.) Alerts Window Message Comments FPL WPT MOVE – Flight plan waypoint moved. T he system has detected that a waypoint coordinate has changed due to a new aviation database update .
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-17 SECTION 12 – ANNUNCIA TIONS & ALERTS Miscellaneous Message Advisories (Cont.) Alerts Window Message Comments SLCT A UT OSEQ – Select auto sequence mode . T he system notifies the pilot to select auto-sequence mode.
Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-18 SECTION 12 – ANNUNCIA TIONS & ALERTS Blank P age.
Garmin G1000 Cockpit Reference Guide for the D A40/40F Index-1 INDEX A Abnormal COM operation 11-2 Activate a flight plan 8-3 Active flight plan 8-2 ADF 1-5, 4-3 ADVISOR Y 12-1 Advisory alerts 12-3 .
Garmin G1000 Cockpit Reference Guide for the D A40/40F Index-2 INDEX HSI 2-5 Hurricanes 10-3 I ICAO 4-5 ID 4-3 IDENT function 4-5 Imminent T errain Impact 10-10 Impact point 10-10 INC FUEL 3-3 Inhibit.
Garmin G1000 Cockpit Reference Guide for the D A40/40F Index-3 INDEX T ropical storms 10-3 TX 4-3 U Unlighted obstacle 10-11 V V ertical Deviation/Glideslope indicator 2-5 V ertical navigation profil.
Garmin G1000 Cockpit Reference Guide for the D A40/40F Index-4 INDEX Blank P age..
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190-00324-06 Rev . A Garmin International, Inc. 1200 East 151st Street Olathe , KS 66062, U .S .A. p: 913.397.8200 f: 913.397.8282 Garmin A T , Inc. 2345 T urner Road SE Salem, OR 97302, U .S .A. p: 503.391.3411 f: 503.364.2138 Garmin (Europe) Ltd. Unit 5, The Quadrangle Abbey P ark Industrial Estate Romsey , SO51 9DL, U .
Un punto importante, dopo l’acquisto del dispositivo (o anche prima di acquisto) è quello di leggere il manuale. Dobbiamo farlo per diversi motivi semplici:
Se non hai ancora comprato il Garmin DA40F è un buon momento per familiarizzare con i dati di base del prodotto. Prime consultare le pagine iniziali del manuale d’uso, che si trova al di sopra. Dovresti trovare lì i dati tecnici più importanti del Garmin DA40F - in questo modo è possibile verificare se l’apparecchio soddisfa le tue esigenze. Esplorando le pagine segenti del manuali d’uso Garmin DA40F imparerai tutte le caratteristiche del prodotto e le informazioni sul suo funzionamento. Le informazioni sul Garmin DA40F ti aiuteranno sicuramente a prendere una decisione relativa all’acquisto.
In una situazione in cui hai già il Garmin DA40F, ma non hai ancora letto il manuale d’uso, dovresti farlo per le ragioni sopra descritte. Saprai quindi se hai correttamente usato le funzioni disponibili, e se hai commesso errori che possono ridurre la durata di vita del Garmin DA40F.
Tuttavia, uno dei ruoli più importanti per l’utente svolti dal manuale d’uso è quello di aiutare a risolvere i problemi con il Garmin DA40F. Quasi sempre, ci troverai Troubleshooting, cioè i guasti più frequenti e malfunzionamenti del dispositivo Garmin DA40F insieme con le istruzioni su come risolverli. Anche se non si riesci a risolvere il problema, il manuale d’uso ti mostrerà il percorso di ulteriori procedimenti – il contatto con il centro servizio clienti o il servizio più vicino.
