Garmin DA40F manuel d'utilisation
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Un bon manuel d’utilisation
Les règles imposent au revendeur l'obligation de fournir à l'acheteur, avec des marchandises, le manuel d’utilisation Garmin DA40F. Le manque du manuel d’utilisation ou les informations incorrectes fournies au consommateur sont à la base d'une plainte pour non-conformité du dispositif avec le contrat. Conformément à la loi, l’inclusion du manuel d’utilisation sous une forme autre que le papier est autorisée, ce qui est souvent utilisé récemment, en incluant la forme graphique ou électronique du manuel Garmin DA40F ou les vidéos d'instruction pour les utilisateurs. La condition est son caractère lisible et compréhensible.
Qu'est ce que le manuel d’utilisation?
Le mot vient du latin "Instructio", à savoir organiser. Ainsi, le manuel d’utilisation Garmin DA40F décrit les étapes de la procédure. Le but du manuel d’utilisation est d’instruire, de faciliter le démarrage, l'utilisation de l'équipement ou l'exécution des actions spécifiques. Le manuel d’utilisation est une collection d'informations sur l'objet/service, une indice.
Malheureusement, peu d'utilisateurs prennent le temps de lire le manuel d’utilisation, et un bon manuel permet non seulement d’apprendre à connaître un certain nombre de fonctionnalités supplémentaires du dispositif acheté, mais aussi éviter la majorité des défaillances.
Donc, ce qui devrait contenir le manuel parfait?
Tout d'abord, le manuel d’utilisation Garmin DA40F devrait contenir:
- informations sur les caractéristiques techniques du dispositif Garmin DA40F
- nom du fabricant et année de fabrication Garmin DA40F
- instructions d'utilisation, de réglage et d’entretien de l'équipement Garmin DA40F
- signes de sécurité et attestations confirmant la conformité avec les normes pertinentes
Pourquoi nous ne lisons pas les manuels d’utilisation?
Habituellement, cela est dû au manque de temps et de certitude quant à la fonctionnalité spécifique de l'équipement acheté. Malheureusement, la connexion et le démarrage Garmin DA40F ne suffisent pas. Le manuel d’utilisation contient un certain nombre de lignes directrices concernant les fonctionnalités spécifiques, la sécurité, les méthodes d'entretien (même les moyens qui doivent être utilisés), les défauts possibles Garmin DA40F et les moyens de résoudre des problèmes communs lors de l'utilisation. Enfin, le manuel contient les coordonnées du service Garmin en l'absence de l'efficacité des solutions proposées. Actuellement, les manuels d’utilisation sous la forme d'animations intéressantes et de vidéos pédagogiques qui sont meilleurs que la brochure, sont très populaires. Ce type de manuel permet à l'utilisateur de voir toute la vidéo d'instruction sans sauter les spécifications et les descriptions techniques compliquées Garmin DA40F, comme c’est le cas pour la version papier.
Pourquoi lire le manuel d’utilisation?
Tout d'abord, il contient la réponse sur la structure, les possibilités du dispositif Garmin DA40F, l'utilisation de divers accessoires et une gamme d'informations pour profiter pleinement de toutes les fonctionnalités et commodités.
Après un achat réussi de l’équipement/dispositif, prenez un moment pour vous familiariser avec toutes les parties du manuel d'utilisation Garmin DA40F. À l'heure actuelle, ils sont soigneusement préparés et traduits pour qu'ils soient non seulement compréhensibles pour les utilisateurs, mais pour qu’ils remplissent leur fonction de base de l'information et d’aide.
Table des matières du manuel d’utilisation
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Page 1
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 0369.11 or later for the Diamond DA40, DA40F . Some differences in operation may be observed when comparing the information in this manual to earlier or [...]
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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[...]
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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[...]
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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[...]
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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[...]
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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 .............................[...]
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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 .......................................................[...]
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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 ................................................[...]
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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[...]
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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[...]
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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[...]
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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[...]
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Page 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[...]
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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[...]
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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[...]
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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[...]
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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[...]
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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[...]
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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[...]
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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[...]
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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[...]
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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[...]
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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[...]
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Page 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[...]
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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[...]
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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?[...]
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Page 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[...]
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Page 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[...]
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Page 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[...]
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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[...]
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Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 3 – ENGINE INDICA TION SYSTEM (EIS) 3-4 Blank P age[...]
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Page 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[...]
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Page 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[...]
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Page 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[...]
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Page 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[...]
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Page 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 [...]
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Page 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[...]
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Page 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 [...]
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Page 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[...]
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Page 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[...]
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Page 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[...]
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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[...]
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Page 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 [...]
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Page 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 [...]
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Page 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[...]
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Page 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 . [...]
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Page 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[...]
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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[...]
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Page 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[...]
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Page 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 [...]
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Page 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[...]
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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[...]
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Page 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[...]
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Page 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[...]
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Page 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[...]
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Page 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 [...]
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Page 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[...]
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Page 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[...]
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Garmin G1000 Cockpit Reference Guide for the D A40/40F SECTION 6 – AUTOMA TIC FLIGHT CONTROL 6-20 Blank P age[...]
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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[...]
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Page 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[...]
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Page 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[...]
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Page 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[...]
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Page 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[...]
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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[...]
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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[...]
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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[...]
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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 [...]
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Page 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[...]
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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[...]
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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[...]
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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[...]
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Page 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[...]
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Page 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[...]
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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[...]
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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[...]
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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[...]
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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[...]
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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 [...]
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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[...]
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Page 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[...]
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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)[...]
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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[...]
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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[...]
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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[...]
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Page 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 [...]
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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[...]
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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[...]
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Page 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 [...]
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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[...]
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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[...]
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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[...]
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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[...]
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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) ?[...]
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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[...]
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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[...]
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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[...]
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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[...]
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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 [...]
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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[...]
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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[...]
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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[...]
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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 [...]
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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[...]
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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[...]
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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[...]
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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 [...]
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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[...]
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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[...]
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Page 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 . [...]
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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[...]
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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[...]
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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[...]
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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 –[...]
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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[...]
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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[...]
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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 [...]
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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[...]