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Garmin DA40F manuale d’uso - BKManuals

Garmin DA40F manuale d’uso

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Un buon manuale d’uso

Le regole impongono al rivenditore l'obbligo di fornire all'acquirente, insieme alle merci, il manuale d’uso Garmin DA40F. La mancanza del manuale d’uso o le informazioni errate fornite al consumatore sono la base di una denuncia in caso di inosservanza del dispositivo con il contratto. Secondo la legge, l’inclusione del manuale d’uso in una forma diversa da quella cartacea è permessa, che viene spesso utilizzato recentemente, includendo una forma grafica o elettronica Garmin DA40F o video didattici per gli utenti. La condizione è il suo carattere leggibile e comprensibile.

Che cosa è il manuale d’uso?

La parola deriva dal latino "instructio", cioè organizzare. Così, il manuale d’uso Garmin DA40F descrive le fasi del procedimento. Lo scopo del manuale d’uso è istruire, facilitare lo avviamento, l'uso di attrezzature o l’esecuzione di determinate azioni. Il manuale è una raccolta di informazioni sull'oggetto/servizio, un suggerimento.

Purtroppo, pochi utenti prendono il tempo di leggere il manuale d’uso, e un buono manuale non solo permette di conoscere una serie di funzionalità aggiuntive del dispositivo acquistato, ma anche evitare la maggioranza dei guasti.

Quindi cosa dovrebbe contenere il manuale perfetto?

Innanzitutto, il manuale d’uso Garmin DA40F dovrebbe contenere:
- informazioni sui dati tecnici del dispositivo Garmin DA40F
- nome del fabbricante e anno di fabbricazione Garmin DA40F
- istruzioni per l'uso, la regolazione e la manutenzione delle attrezzature Garmin DA40F
- segnaletica di sicurezza e certificati che confermano la conformità con le norme pertinenti

Perché non leggiamo i manuali d’uso?

Generalmente questo è dovuto alla mancanza di tempo e certezza per quanto riguarda la funzionalità specifica delle attrezzature acquistate. Purtroppo, la connessione e l’avvio Garmin DA40F non sono sufficienti. Questo manuale contiene una serie di linee guida per funzionalità specifiche, la sicurezza, metodi di manutenzione (anche i mezzi che dovrebbero essere usati), eventuali difetti Garmin DA40F e modi per risolvere i problemi più comuni durante l'uso. Infine, il manuale contiene le coordinate del servizio Garmin in assenza dell'efficacia delle soluzioni proposte. Attualmente, i manuali d’uso sotto forma di animazioni interessanti e video didattici che sono migliori che la brochure suscitano un interesse considerevole. Questo tipo di manuale permette all'utente di visualizzare tutto il video didattico senza saltare le specifiche e complicate descrizioni tecniche Garmin DA40F, come nel caso della versione cartacea.

Perché leggere il manuale d’uso?

Prima di tutto, contiene la risposta sulla struttura, le possibilità del dispositivo Garmin DA40F, l'uso di vari accessori ed una serie di informazioni per sfruttare totalmente tutte le caratteristiche e servizi.

Dopo l'acquisto di successo di attrezzature/dispositivo, prendere un momento per familiarizzare con tutte le parti del manuale d'uso Garmin DA40F. Attualmente, sono preparati con cura e tradotti per essere comprensibili non solo per gli utenti, ma per svolgere la loro funzione di base di informazioni e di aiuto.

Sommario del manuale d’uso

  • Pagina 1

    Integr ated Flight Deck Cockpit Refer ence Guide Diamond DA40/40F[...]

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    [...]

  • Pagina 3

    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 0369.11 or later for the Diamond DA40, DA40F . Some differences in operation may be observed when comparing the information in this manual to earlier or [...]

  • Pagina 4

    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. T he G1000 T errain Proximity feature is NO T intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the respo[...]

  • Pagina 5

    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 . However , the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical[...]

  • Pagina 6

    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. Depictions of equipment may differ slightly from the actual equipment[...]

  • Pagina 7

    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 Added Flight T imer Added extended range fuel tanks Changed NA V1 and NA V2 on the PFD to VOR or LOC Moved altitude and airspeed trend vectors to opposit[...]

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    Garmin G1000 Cockpit Reference Guide for the D A40/40F RECORD OF REVISIONS RR-2 Blank P age[...]

  • Pagina 9

    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 ............................................................ 1-4 1.3 MFD Softkeys .............................[...]

  • Pagina 10

    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 ....................... 6-13 Departure .......................................................[...]

  • Pagina 11

    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 ...................... 8-4 8.8 Load a Departure ................................................[...]

  • Pagina 12

    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 .................................. 12-10 GMA 1347 Message Advisories ............................... 12-11 GIA 6[...]

  • Pagina 13

    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 . It is not intended to be a comprehensive operating gui[...]

  • Pagina 14

    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 700) 17 26 25 24 27 18 19 23 22 21 20[...]

  • Pagina 15

    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. Press to turn the Morse code identifier ON and OFF . V olu[...]

  • Pagina 16

    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. (17) Dual AL T Knob – Sets the selected altitude in the box located above t[...]

  • Pagina 17

    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. XM L TNG BACK ALERTS (optional) (optional) Figure 1-3 PFD Softkey Flow Chart – 1 PFD Press the STD BARO or BACK Softkey to r[...]

  • Pagina 18

    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. ALER TS – Press to display the Alerts W indow . Press the BACK Softkey to return to th[...]

  • Pagina 19

    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 . ALER TS – Press to display the Alerts Wi[...]

  • Pagina 20

    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. TERRAIN – Pressing this softkey displays/ removes terrain and obstacle data on t[...]

  • Pagina 21

    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. Figure 1-8 PFD Setup Menu Window 1.6 XM RADIO - AUT OMA TIC MUTING XM Radio audio will be automatically muted when the aircraft gr oundspeed exceeds approximately 30 k[...]

  • Pagina 22

    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. A Supplemental Data Card should be inserted into the bottom car d slot of[...]

  • Pagina 23

    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. 6 7 1 1 14 15 8 13 12 5 3 4 2 1 16 Figure 2-1 Default PFD Information 14 15 1 1 13 12 9 6 4 2 5 16 7 3 1 NA V Frequency Box Airspeed Ind[...]

  • Pagina 24

    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 Course Box Annunciation W indow 7 Alerts W indow V ertical Deviation/Glideslope Indicator Marker Beacon Annunciation Selected Heading Box 5 10 DME Inf[...]

  • Pagina 25

    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 Box Speed Ranges (low end yellow band not displayed and other low end speed ranges differ on EASA certified air craft) Vspeed Refer ences Speed Indicat[...]

  • Pagina 26

    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 2-7 Altimeter Altitude Select Bug Altitude Select Bug The Altitude Select Bug is displayed at the selected altitude or , if the selected altitude is b[...]

  • Pagina 27

    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 2.4 MARKER BEACON ANNUNCIA TIONS Figure 2-10 Marker Beacon and V ertical Deviation Marker[...]

  • Pagina 28

    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 urn Rate Indicator Navigation Source Course Deviation Indicator TO/FROM Indicator Course Pointer Rotating Compass Rose 1 1 10 12 13 14 9 8 OBS Mode L[...]

  • Pagina 29

    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. See System Setup in the G1000 Pilot?[...]

  • Pagina 30

    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 present or is invalid for navigation use • W ARN – GPS detects a position error • SUSP – Displayed when in OBS Mode indicating GPS waypoint seq[...]

  • Pagina 31

    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. Pressing the ENGINE Softkey makes available the LEAN and SYSTEM Softkeys which in[...]

  • Pagina 32

    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 . The CYL SLCT Softkey becomes disabled when a particular cylinder tur ns yellow or red, until the temperature decr e[...]

  • Pagina 33

    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. NO TE: Fuel calculations do not use the aircraft fuel quantity indicators, and are calcul[...]

  • Pagina 34

    Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 3 – ENGINE INDICA TION SYSTEM (EIS) 3-4 Blank P age[...]

  • Pagina 35

    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. NA V Contr ols COM Contr ols NA V Fr equency Box COM Fr equency Box Figure 4[...]

  • Pagina 36

    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 Fr equency Field Figure 4-2 Frequency Fields Selected NA V Fr equency T uning Box T uning Box Selected COM Fr equency Fr equency T ransfer Arr ow T uni[...]

  • Pagina 37

    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. • TX – When a CO M radi o is tr ans mit ti ng, a whit e ‘TX’ indication appears to the rig[...]

  • Pagina 38

    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 . 2 ) T urn the small F M S Knob to display the selection window . T urn the[...]

  • Pagina 39

    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. Figure 4-11 Ground Mode Reply Status When the transponder send[...]

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    Garmin G1000 Cockpit Reference Guide for the D A40/40F 4-6 SECTION 4 – NA V/COM & TRANSPONDER Blank P age[...]

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    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 COM (Unavailable) T elephone (Unavailable) Marker Beacon/Mute Passenger Addr ess Marker Beacon Signal Sensitivity Speaker VOL/SQ V olume/Squelch Manual [...]

  • Pagina 42

    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. T o prevent deselecting the desired received audi[...]

  • Pagina 43

    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. Figure 5-6 ICS Isolation Mode PILOT KEY ANNUNCIA TOR COPL T KEY ANNUNCIA [...]

  • Pagina 44

    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. Once the 2.5 minutes of r ecording ti[...]

  • Pagina 45

    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. In addition to the AFCS (Automatic F[...]

  • Pagina 46

    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 Mode System Status Annuciation (see Annunciations & Alerts) Flight Dir ector Command Bars AFCS Status Box Air craft Attitude Symbol Selected Alti[...]

  • Pagina 47

    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. Also, the autopilot disconne[...]

  • Pagina 48

    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. T he system will maintain or give command bar direction for a constant pitch attitude (pitch reference) depending [...]

  • Pagina 49

    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 . T he fligh t dire cto r is act iv ate d (if not alrea dy activ e) and ‘ AL T’ is now displ aye d in green in the Active Mode Field with the current altitude displayed in the Altitude Reference [...]

  • Pagina 50

    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 . Pitc[...]

  • Pagina 51

    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 . [...]

  • Pagina 52

    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 . Subsequent autopilot e[...]

  • Pagina 53

    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. AFCS K ey AFCS Mode Annunciation FD/AP only Roll Hold (Default) ROL HDG Heading Select HDG NA V VOR Enroute Arm / Capture / T rack VOR GPS A[...]

  • Pagina 54

    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. T he selected heading w[...]

  • Pagina 55

    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.g. GPS, VOR or LOC). GPS roll steering commands are followed when the [...]

  • Pagina 56

    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. The Ap[...]

  • Pagina 57

    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. In this scenario, the aircraft departs Reid-Hillview Airport (KRHV) from runway 13L, enr oute to Fresno[...]

  • Pagina 58

    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 . T o have the autopilot capture this altitude , use Pitch Hold, Ve rtical Speed, or Flight Level Cha[...]

  • Pagina 59

    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. Airway V107 to Panoch[...]

  • Pagina 60

    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. 2) T ransition from VOR to GPS Navigation Mode . a) Use the CDI Softk ey to put the HSI in GPS mo[...]

  • Pagina 61

    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 . 1) Enter Flight Level Change Mode . a) Using the AL [...]

  • Pagina 62

    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. b) Select ‘V ectors to Final’ for the tr ansition. c) Set the Selected Heading after getting v[...]

  • Pagina 63

    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 . Not e that when the GA but ton is pu shed , t he auto[...]

  • Pagina 64

    Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-20 Blank P age[...]

  • Pagina 65

    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. 7.1 NA VIGA TION MAP P AGE Select the MAP Page Gr oup 1 ) T urn the large FMS Knob until ‘ MAP’ is highligh ted in the P age Group Box in the[...]

  • Pagina 66

    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. 5) Press the ENT K ey to confirm the selection. Press ENT again to activate a[...]

  • Pagina 67

    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. Enter a W aypoint F acility N[...]

  • Pagina 68

    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. Figure 7-6 Intersection Information P age Access Inform[...]

  • Pagina 69

    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. Access Information on a VOR 1) Wit h th[...]

  • Pagina 70

    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. 2) T urn the small FMS Knob to s[...]

  • Pagina 71

    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 . 2) T urn the small FMS Knob to select the second rectangular page icon. View Information on[...]

  • Pagina 72

    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. Figure 7-13 Nearest VOR P age View Information on the Near est VOR 1) With the Ne[...]

  • Pagina 73

    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 . 2) T urn the small FMS Knob to select the [...]

  • Pagina 74

    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. 3) Press the ALER TS Softk ey to pla[...]

  • Pagina 75

    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. 8.1 USER DEFINED WA YPOINTS Figure 8-1 User WPT Information P age Select the User WPT Information Page 1) T urn the large FMS Knob to selec[...]

  • Pagina 76

    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. 2) Move the Joystick to place the pointer at t[...]

  • Pagina 77

    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. 2) Press the A CT LEG Softk ey (using MFD only). OR 3) Press the MENU K[...]

  • Pagina 78

    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 . 4) T urn the small FMS Knob to enter the first c[...]

  • Pagina 79

    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. 8.11 REMO VE A DEP ARTURE, ARRIV AL, OR APPROA CH FROM A FLIGHT PLAN 1) With the Active or Stored Flight Plan Page displayed, press the FMS Knob[...]

  • Pagina 80

    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. 3) Press the INVER T Softk ey . ‘Invert and activ ate st[...]

  • Pagina 81

    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 .P OS’ (p re se nt po si ti on ). If nec ess ar y , press the MENU K ey and sel[...]

  • Pagina 82

    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. Figure 8-16 V ertical Navigation (VNA V) P age Create a V ert[...]

  • Pagina 83

    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. 11) Press the ENT Key . T he cursor is n[...]

  • Pagina 84

    Garmin G1000 Cockpit Reference Guide for the D A40/40F 8-10 SECTION 8 – FLIGHT PLANNING Blank P age[...]

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    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 . If a fligh t plan is activ e , the departure airport will be displayed [...]

  • Pagina 86

    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 . Figure 9-4 Select Arrival T ransition 7) A thir d win dow is disp lay ed list ing[...]

  • Pagina 87

    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 . (T he “V ec tor s” opti on ass ume s vect ors will be received to the final course segment of the appr oach and wi[...]

  • Pagina 88

    Garmin G1000 Cockpit Reference Guide for the D A40/40F 9-4 SECTION 9 – PROCEDURES Blank P age[...]

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    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. The cursor flashes on the ‘Map Setup’ option. 2)[...]

  • Pagina 90

    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). Figure 10-5 MET AR and T AF T ext Displayed on the Airport (W eather) Information P age MET AR T ext T AF T ext WX Softkey Displaying Weather[...]

  • Pagina 91

    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. ECHO TOPS cannot be displayed along with NEXRAD and CLOUD[...]

  • Pagina 92

    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. Panning over an airport with MET AR informat ion does not display more information but allows the user to press the ENT[...]

  • Pagina 93

    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 W arnings 60 Echo T ops 30 F reezing Levels 60 MET ARs 90 Lightning 30 NEXRAD 30 Radar Coverage 30 Cell Movement 30 Surface Analysis 60 TFRs 60 Winds [...]

  • Pagina 94

    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 raffic Mode Figure 10-8 T raffic Map P age Pr oximity T raffic at same altitude, level flight & moving in the dir ection of the line T raffic Advi[...]

  • Pagina 95

    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 . 1000' Aircraft Altitude 100' Threshold Unlighted[...]

  • Pagina 96

    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. NO TE: T AWS ope rat ion is only ava ila ble when the G1000 is [...]

  • Pagina 97

    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 . Y ellow T errain/Obstacle between 100’ and 1000’ below current[...]

  • Pagina 98

    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. The system test may also be initiated manually , but on ly whe n the ai rc raf t is o[...]

  • Pagina 99

    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. EDR alerts have two levels of severity , caution (sink rate) and warning (p[...]

  • Pagina 100

    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. Figure 10-18 Alert P op-Up Press the ENT Key to display the T A WS Page, or press the CLR Key to re[...]

  • Pagina 101

    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. Alert T ype PFD/MFD T A WS P age Annunciation MFD P op-Up Alert Aural Message Exc ess ive Des cen t R ate W arnin g ( EDR) ?[...]

  • Pagina 102

    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. Alert T ype PFD/MFD T A WS P age Annunciation MFD P op-Up Alert Aural Message T AW S S yst em T est F ail None “T A WS Sys tem F ailur e” T AW S Alert ing is di sabl ed None None No GPS po s[...]

  • Pagina 103

    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. In reversionary mode, critical flight instrumentation is combined with engine instrumenta[...]

  • Pagina 104

    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. In the event of a[...]

  • Pagina 105

    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. Figure 12-1 G1000 Alerting System Annunciation Window Alerts Window ALERTS Softkey Annunciation System Annunciatio[...]

  • Pagina 106

    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. 12.1 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in [...]

  • Pagina 107

    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. WARNING Alerts Annunciation Window T ext Alerts Window Message Aud[...]

  • Pagina 108

    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 . AP is inoperative . Roll F ailur[...]

  • Pagina 109

    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. Pop-up alerts appear only on the MFD. Alert T ype PFD/MFD T A WS P age Annunciation MFD Map P age P op-Up Alert Aural Message Exc ess ive Des cen t R ate W arnin g ( EDR) “Pu ll Up” Re[...]

  • Pagina 110

    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 Aural Message T AW S S yst em T est F ail None “T A WS Sys tem F ailur e” T AW S Alert ing is di sabl ed None None No GPS po siti on or exc essi [...]

  • Pagina 111

    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 . Display is not receiving vertical speed input from the air data computer . Dis[...]

  • Pagina 112

    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. The Figure 12-6 illustrates all possible flags and the responsible LRUs. Figure 12-6 G1000 System F ailure Annunciations GDC 74A Air Data Computer GTX 33 T ransponder OR GIA 6[...]

  • Pagina 113

    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. T he pilot may reconfigure the MFD & PF[...]

  • Pagina 114

    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. Attempt to reload the aviation database . If problem persists , the [...]

  • Pagina 115

    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. Crossfill is off . Install correct airport[...]

  • Pagina 116

    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. T he G1000 system should be serviced. GIA2 SE[...]

  • Pagina 117

    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 . GPS1 F AIL – GPS1 is inoperative . [...]

  • Pagina 118

    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 . T he G1000 system should be s[...]

  • Pagina 119

    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. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. T he G1000 system sho[...]

  • Pagina 120

    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 . V erify that stored flig[...]

  • Pagina 121

    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. Press the OBS Softk ey to deactivate the OBS mode . SLCT FREQ –[...]

  • Pagina 122

    Garmin G1000 Cockpit Reference Guide for the D A40/40F 12-18 SECTION 12 – ANNUNCIA TIONS & ALERTS Blank P age[...]

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    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 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 inform[...]

  • Pagina 124

    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 10-9 Inhibit T AWS 10-9 INTEG 2-8 Interrogations 4-5 IOI 10-10, 10-13, 12-5 ITI 10-10 K K ey(s) 1-4 L Lean engine 3-2 Lighted obstacle 10-11 Load app[...]

  • Pagina 125

    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 profile 8-8 V ertical speed 1-4, 2-5, 6-3, 6-6 V ertical Speed Bug 2-5 V ertical Speed Mode 6-6 VFR code 4-5 VHF 4-1 VOL/PUSH ID 4-2 VOL/PUSH SQ 4-2, 4-3 V [...]

  • Pagina 126

    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 .K. p: 44/0870.8501241 f: 4[...]