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G1000

Pilot’s Guide

for the Diamond DA40

Summary of content (338 pages)

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G1000 TM Pilot’s Guide for the Diamond DA40
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Part Number 190-00592-00 (Rev. A) Change Summary Reformatted for single part number (all previous part numbers incorporated into this part number) Added optional fuel pressure indicator information Record of Revisions Revision Date of Revision Revision Page Range A 11/10/05 i through I-6 Description Initial release. Garmin G1000 Pilot’s Guide For the Diamond DA40 190-00592-00 Rev.
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COPYRIGHT Copyright © 2005 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reﬂects the operation of System Software version 0369.09 or later for the DA40, DA40F and System Software version 0370.13 or later for the DA40D. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc.
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WARNINGS & CAUTIONS WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during ﬂight. The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certiﬁed for use in applications requiring a certiﬁed terrain awareness system.
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WARNINGS & CAUTIONS CAUTION: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 can be misused or misinterpreted and, therefore, become unsafe.
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WARRANTY LIMITED WARRANTY This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost.
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TABLE OF CONTENTS 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1 – SYSTEM OVERVIEW System Description......................................... 1-1 LRU Descriptions ............................................ 1-1 PFD/MFD Controls ......................................... 1-6 Secure Digital Cards ....................................... 1-8 System Power-up ............................................ 1-9 Display Backlighting ......................................1-11 System Operation ........................................
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TABLE OF CONTENTS 3.5 Frequency Auto-Tuning ..................................3-13 Reversionary Mode ....................................................5-9 Auto-Tuning on the PFD ...........................................3-13 Auto-Tuning on the MFD ..........................................3-14 Auto-Tuning Upon Approach Activation (NAV Frequencies) .............................................................3-20 6 – ENGINE INDICATION SYSTEM 6.1 Introduction............................................
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TABLE OF CONTENTS Active Flight Plan Page .............................................7-39 Active Flight Plan Page Options ...............................7-40 Flight Plan Catalog Page ..........................................7-49 Flight Plan Catalog Page Operations .......................7-49 Vertical Navigation (VNAV) Page..............................7-55 7.7 Procedures .....................................................7-57 Arrivals and Departures ............................................
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TABLE OF CONTENTS Appendix C Questions & Answers ........................ C-1 Appendix D G1000 Map Datums .......................... D-1 Appendix E General TIS Information .................... E-1 Introduction................................................................E-1 TIS vs. TCAS ................................................................E-1 TIS Limitations ............................................................E-1 Appendix F Map Symbols .....................................
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G1000 TM System Overview
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Garmin G1000 Pilot’s Guide for the Diamond DA40 190-00592-00 Rev.
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SYSTEM OVERVIEW 1.1 SYSTEM DESCRIPTION This section provides an overview of the G1000 Integrated Cockpit System as installed in the Diamond DA40 aircraft.
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SYSTEM OVERVIEW • GIA 63 – The GIA 63s are the central Integrated Avionics Units (IAUs) of the G1000 System. The IAUs serve as the main communications hub, linking all LRUs with the PFD and the MFD displays. Each IAU contains a GPS receiver, VHF COM/NAV/GS receivers, and system integration microprocessors and is paired with a GDU 1040 display through an Ethernet connection. The IAUs do not communicate with each other directly.
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SYSTEM OVERVIEW • GEA 71 – The GEA 71 receives and processes signals from the engine and airframe sensors. Sensor types include engine temperature and pressure sensors as well as fuel measurement and pressure sensors. The Engine/Airframe Unit communicates with both IAUs using an RS-485 digital interface. • GDL 69/69A – The GDL 69/69A is an XM satellite radio receiver that provides real-time weather information to the MFD and PFD Inset Map. The Data Link also provides digital audio entertainment.
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SYSTEM OVERVIEW High-Speed Data Bus (Ethernet) GMA 1347 Audio Panel GDU 1040 (PFD) GDU 1040 (MFD) Reversionary Control Reversionary Control GDC 74A Air Data Computer No. 1 GIA 63 Integrated Avionics Unit System Inegration Processors I/O Processors VHF COM VHF NAV/LOC GPS Glideslope GPS Output OAT Airspeed Altitude Vertical Speed GRS 77 AHRS Attitude Rate of Turn Slip/Skid No.
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SYSTEM OVERVIEW �� Figure 1-2 G1000 Optional Features NOTE: For information on optional equipment shown in the
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SYSTEM OVERVIEW 1.
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SYSTEM OVERVIEW The G1000 controls and keys have been designed to simplify the operation of the system and to minimize workload as well as the time required to access sophisticated functionality. The following list provides an overview of the primary function(s) of the keys and knobs located on the display bezel. 1 NAV VOL/ID Knob – Controls the NAV audio level 6 CRS/BARO Knob – The large knob sets the altimeter barometric pressure and the small knob adjusts the course.
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SYSTEM OVERVIEW 13 To immediately display the Navigation Map Page, press and hold the CLR key (MFD only). 14 Dual FMS (Flight Management System) Knobs – Used to select the page to be viewed (only on the MFD) The large knob selects a page group (MAP, WPT, AUX, NRST) while the small knob selects a speciﬁc page within the page group. Pressing the small knob turns the selection cursor ON and OFF.
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SYSTEM OVERVIEW 1.5 SYSTEM POWER-UP The G1000 System is integrated with the aircraft electrical system and receives power directly from electrical busses. The Garmin G1000 PFD/MFD and supporting sub-systems include both power-on and continuous builtin test features that exercise the processor, RAM, ROM, external inputs, and outputs to provide safe operation. While the system begins to initialize, test annunciations are displayed on the PFD at power-up.
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SYSTEM OVERVIEW When the MFD powers up, the MFD Power-up page displays the following data: • • • • • • • System version Copyright Checklist ﬁlename Land database name and version Obstacle database name and version Terrain database name and version Aviation database name, version, and effective dates When this information has been reviewed for currency (to ensure that no databases have expired), the pilot is prompted to continue.
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SYSTEM OVERVIEW 1.6 DISPLAY BACKLIGHTING NOTE: Refer to the Primary Flight Display section for instructions on manually adjusting the backlighting. The G1000 PFD and MFD displays use photocell technology to automatically adjust for ambient lighting conditions. Photocell calibration curves are pre-conﬁgured to optimize display appearance through a broad range of cockpit lighting conditions.
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SYSTEM OVERVIEW REVERSIONARY MODE Should a failure occur in either display, the G1000 automatically enters reversionary mode. In reversionary mode, all important ﬂight information is shown on the remaining display. Figure 1-7 shows an example of G1000 reversionary mode where the PFD has failed. If a display fails, the appropriate GIA 63-GDU 1040 Ethernet interface is cut off.
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SYSTEM OVERVIEW AHRS MODES OF OPERATION GPS Input Failure The GRS 77 Attitude and Heading Reference System (AHRS) performs attitude, heading, and vertical acceleration calculations for the G1000 System utilizing GPS, Magnetometer, and air data in addition to information from its internal sensors. Attitude and heading information are updated on the PFD while the AHRS receives appropriate combinations of information from the external sensor inputs (see Figure 1-8).
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SYSTEM OVERVIEW 1.8 CHECKLISTS (OPTIONAL) The G1000 MFD is able to display electronic checklists customized for the Diamond DA40. The G1000 accesses the checklists from an SD card inserted into the bezel slot (see Figure 1-3). Pressing the CHKLIST softkey allows access to all checklists. Pressing the EXIT softkey exits the Checklist pages and displays the page last viewed.
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G1000 TM Primary Flight Display
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Garmin G1000 Pilot’s Guide for the Diamond DA40 190-00592-00 Rev.
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PRIMARY FLIGHT DISPLAY 2.1 INTRODUCTION WARNING: In the event that the airspeed, attitude, altitude, or heading indications become unusable, please refer to the backup instruments. This section describes the major features of the G1000 Primary Flight Display (PFD) as installed on Diamond DA40, DA40F, and DA40D aircraft. Information is displayed using the G1000’s two 10.4-inch color ﬂat-panel displays. During normal operation, the left display is conﬁgured as a Primary Flight Display.
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PRIMARY FLIGHT DISPLAY 1 18 17 16 15 14 2 13 12 3 11 4 10 9 5 6 8 7 1 NAV Frequency Window 10 Turn Rate Indicator 2 Airspeed Indicator 11 Barometric Setting Box 3 True Airspeed Box 12 Vertical Speed Indicator 4 Heading Box 13 Altimeter 5 Horizontal Situation Indicator 14 Altitude Reference Box 6 Outside Air Temperature Box 15 COM Frequency Window 7 Softkeys 16 Navigation Status Bar 8 System Time Box 17 Slip/Skid Indicator 9 Transponder Status Bar 18 Attitude
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PRIMARY FLIGHT DISPLAY 12 1 11 10 9 2 8 3 7 6 5 4 1 Trafﬁc Annunciation 7 Auxiliary Window (Radio Tuning Window) 2 Selected Heading Box 8 Selected Course Box 3 Inset Map 9 Annunciation Window 4 BRG1 Information Window 10 Vertical Speed Pointer 5 DME Information Window 11 Vertical Deviation/Glideslope Indicator 6 BRG2 Information Window 12 Marker Beacon Annunciation Figure 2-2 Additional PFD Information 190-00592-00 Rev.
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PRIMARY FLIGHT DISPLAY 2.2 BACKLIGHTING NOTE: The backlighting can only be adjusted from the PFD, except in reversionary mode. NOTE: No other window can be displayed in the lower right corner of the PFD when the MENU key is pressed to change the backlighting. The backlighting of both the display and the keys can be adjusted for the PFD and MFD. The backlighting intensity ranges from 0.14% to 100.00%.
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PRIMARY FLIGHT DISPLAY 2.3 SOFTKEY FUNCTION When a softkey is turned on, its color changes to black text on gray background and remains this way until it is turned off, at which time it reverts to white text on black background. The CDI, IDENT, ADF/DME, TMR/REF, NRST, and ALERTS softkeys change momentarily to black text on gray background and automatically switch back to white text on black background.
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PRIMARY FLIGHT DISPLAY • CDI – Changes navigation mode on the CDI to GPS, NAV1, or NAV2 • IDENT – Provides special aircraft position identiﬁcation to ATC • ADF/DME (optional; may appear as ADF, DME, or ADF/DME depending on the installation) – Displays ADF/DME Radio Tuning Window • TMR/REF – Displays Timer/References Window • OBS – Selects OBS mode on the CDI when navigating by GPS (only available with active leg) • NRST – Displays Nearest Airports Window • ALERTS – Displays Alerts Window • XPDR – Disp
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PRIMARY FLIGHT DISPLAY �� Figure 2-5 Top-Level PFD Softkeys �� (��) (��) (��) �� Figure 2-6 INSET Softkeys 190-00592-00 Rev.
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PRIMARY FLIGHT DISPLAY �� Figure 2-7 PFD Conﬁguration Softkeys ��
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PRIMARY FLIGHT DISPLAY 2.4 FLIGHT INSTRUMENTS AIRSPEED INDICATOR The Airspeed indicator displays airspeed on a rolling number gauge, using a moving tape. The following information is also displayed: • • • • Speed indication Speed ranges Airspeed Trend Vector Vspeed References Vspeed References Vspeeds are set using the TMR/REF softkey. Glide, VR, VX, and VY are shown on the References window.
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PRIMARY FLIGHT DISPLAY ATTITUDE INDICATOR The attitude information is displayed over a virtual blue sky and a brown ground with a white horizon line. The Attitude indicator displays the following information: NOTE: Supplemental ﬂight data, such as the Inset Map and the Alerts and Annunciation Windows, disappear from the PFD when pitch exceeds +30˚ or -20˚ or when a 65˚ bank angle is reached.
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PRIMARY FLIGHT DISPLAY Pitch Indication Roll Indication Major pitch marks and numeric labels at 10, 20, 30, 40, 50, 60, 70 and 80 degrees are shown above and below the horizon line. Minor pitch marks at 5, 15 and 25 degrees above the horizon line and 5, 15, 25, 35 and 45 degrees below the horizon line are shown. The horizon line is part of the pitch scale.
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PRIMARY FLIGHT DISPLAY ALTIMETER Altitude Select Bug The Altimeter displays barometric altitude values in feet on a rolling number gauge using a moving tape. The Altimeter displays the following information: The Altitude Select Bug is displayed at the Selected Altitude or the edge of the tape (whichever is closer to the current altitude) to provide increased altitude awareness. This altitude also appears in the Selected Altitude Box above the Altimeter.
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PRIMARY FLIGHT DISPLAY Altitude Alerting Metric Display The altitude Alerting function provides the pilot with a visual alert when approaching the Selected Altitude. This function is independent of the ﬂight control system. Visual annunciations appear in the Selected Altitude box. The Altitude Alerting function is reset whenever the Selected Altitude is adjusted. Selected and current altitude can be displayed in meters in addition to English units.
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PRIMARY FLIGHT DISPLAY VERTICAL DEVIATION/GLIDESLOPE INDICATOR The Vertical Deviation/Glideslope indicator is a window on the left side of the Altimeter. The window appears when an ILS is tuned in the active NAV ﬁeld (and selected on the Audio Panel). A green diamond appears and acts as the vertical deviation indication, just like a glideslope needle on a conventional indicator. MARKER BEACON ANNUNCIATIONS Marker Beacon Annunciations are displayed on the PFD to the left of the Selected Altitude Box.
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PRIMARY FLIGHT DISPLAY HORIZONTAL SITUATION INDICATOR The Horizontal Situation Indicator (HSI) displays a rotating compass card with letters at the cardinal points and numeric labels every 30 degrees. Major tick marks are at 10-degree intervals and minor tick marks at 5 degree intervals. The HSI is displayed in a heading-up orientation. The HSI is available in two formats (360˚ compass rose and 140˚ arc).
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PRIMARY FLIGHT DISPLAY Heading Indication Arc HSI NOTE: When the Arc HSI is displayed the BRG1 and BRG2 Information Windows and pointers are disabled. NOTE: If the pilot makes a heading change greater than 105˚ with respect to the course, the CDI switches to the opposite side of the deviation scale and displays reverse sensing. The Arc HSI is a 140˚ expanded section of the compass rose.
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PRIMARY FLIGHT DISPLAY Turn Rate Indicator Course Deviation Indicator The Turn Rate Indicator is located directly above the rotating compass card. Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta turn rate trend vector shows the current turn rate. The end of the trend vector gives the heading predicted in six seconds, based on the present turn rate.
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PRIMARY FLIGHT DISPLAY Bearing Pointers and Information Windows Up to two bearing pointers can be displayed on the HSI. Pressing the PFD softkey provides access to the BRG1 and BRG2 softkeys. The BRG1 pointer is a single cyan line with an open arrowhead at the end. The BRG2 pointer is a double cyan line with an open arrowhead at the end. The bearing pointers never override the CDI.
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PRIMARY FLIGHT DISPLAY DME Radio (optional) ADF Radio (optional) The DME radio is a Honeywell KN63 remote mounted, 200-channel, 100-watt, all-solid-state digital DME which provides distance information to the G1000. The ADF radio is a Becker RA3502 (1) remote mounted ADF radio receiver that operates in the frequency range 190.0 to 1799.5 kHz in 0.5 kHz increments. Press the PFD softkey followed by the DME softkey to display the DME Information Window.
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PRIMARY FLIGHT DISPLAY Radio Tuning Window (optional) NOTE: The Radio Tuning window is only available if the DME and/or ADF radios are installed. The Radio Tuning window is displayed by pressing the ADF/DME (ADF, DME, or ADF/DME depending on the installation) softkey. This window provides display and control of single or dual ADF and DME radio(s). Depending on the installation, the Radio Tuning window may be titled ADF Tuning, DME Tuning, or ADF/DME Tuning.
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PRIMARY FLIGHT DISPLAY Navigation Source To enable/disable OBS mode while navigating with GPS: NOTE: OBS is only available with the active ﬂight plan leg, when navigating under GPS. The HSI can display two sources of navigation: GPS or NAV (VOR, localizer, and glideslope). In GPS mode, the ﬂight plan legs are sequenced automatically. Enabling OBS mode suspends auto sequencing of waypoints, but retains the current “active-to” waypoint as the navigation reference even after passing the waypoint.
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PRIMARY FLIGHT DISPLAY 2.5 COMMUNICATION, NAVIGATION, & SURVEILLANCE COMMUNICATION FREQUENCY WINDOW The Communication (COM) Frequency Window, located in the upper right corner of the PFD, provides control and display of dual VHF Radio Communication Transceivers (COM1 and COM2).
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PRIMARY FLIGHT DISPLAY NAVIGATION STATUS BAR TRANSPONDER (XPDR) STATUS BAR The Navigation Status bar is located at the top of the PFD and displays valuable information while ﬂying a route: • • • • • The next waypoint in the active ﬂight plan Distance to the next waypoint (DIS) Desired track to the next waypoint (DTK) Current track angle (TRK) GPS Navigation Annunciations NOTE: The ﬁelds in the PFD Navigation Status bar cannot be changed.
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PRIMARY FLIGHT DISPLAY 2.6 SUPPLEMENTAL FLIGHT DATA OUTSIDE AIR TEMPERATURE BOX The outside air temperature (OAT) is displayed in °C with the “OAT” label. °F can be displayed using the AUX System Setup Page on the MFD (refer to the Multi Function Display section). Figure 2-40 Outside Air Temperature Box SYSTEM TIME BOX The System Time box displays the local time. Time and date are obtained from the satellites and cannot be changed. The pilot may select the desired time format and offset.
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PRIMARY FLIGHT DISPLAY The following Inset Map operations can be performed independently of the MFD: • • • • • • • Change zoom range Change declutter level Enable/disable trafﬁc data Enable/disable topographic data Enable/disable terrain data Enable/disable weather information (optional) Pan Map 1 9 2 8 3 7 6 4 5 1 Wind Vector 2 NAV Compass Range 3 NAV Compass 4 Trafﬁc Icon and Scale 5 Map Range Terrain Icon 6 7 8 Active Navigation Route Track Vector 9 Map Orientation Figure 2-42 Inset Ma
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PRIMARY FLIGHT DISPLAY To enable/disable topo data: 1. Press the INSET softkey. 2. Press the TOPO softkey to display topographic land colors, which represent the rise and fall of land elevation. 3. Press the TOPO softkey again to remove topo data from the map. NOTE: When topographic data is removed from the display, all cartographic data is automatically removed and the Jeppesen Nav Data is presented on a black background. To enable/disable terrain data: 1. Press the INSET softkey. 2.
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PRIMARY FLIGHT DISPLAY AUXILIARY WINDOW KEYS The main keys which are used in association with PFD Auxiliary Window operations are listed below: 1 DIRECT-TO – Activates the direct-to function and allows the user to enter a destination waypoint and establishes a direct course to the selected destination (speciﬁed by identiﬁer chosen from the active route) 2 FPL – Displays the active Flight Plan Page for creating and editing the active ﬂight plan or accessing stored ﬂight plans 3 CLR – Erases information
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PRIMARY FLIGHT DISPLAY WORKING WITH MENUS AUXILIARY WINDOWS NOTE: Pressing a softkey does not display a menu or sub-menu. Much G1000 operation is accomplished using a menu interface. The G1000 has a bezel-mounted dedicated MENU key that displays a context-sensitive list of options when pressed. This option list allows the pilot to access additional features or make setting changes speciﬁcally relating to the currently displayed window. There is no all-encompassing menu.
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PRIMARY FLIGHT DISPLAY Generic Timer The Generic Timer displays time (hr:min:sec), timer count direction (UP or DOWN), and timer status (START, STOP, or RESET). To change the Generic Timer: Flight ID Flight status automatic reporting of aircraft identiﬁcation (ID) is transmitted by the transponder to the ground stations and other aircraft. The ﬂight ID is set to ﬁxed (“SAME AS TAIL” and “CONFIG ENTRY”) or variable (“PFD ENTRY”) at the time of installation.
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PRIMARY FLIGHT DISPLAY Vspeeds and Vspeed Bug Status NOTE: Default settings are automatically restored when power is cycled. Vspeed values for the aircraft can be found in the Aircraft Flight Manual (AFM). The Vspeeds can be changed and the Vspeed bugs can be turned ON or OFF: To change Vspeeds and turn the Vspeed bug ON or OFF: 1. Press the TMR/REF softkey, then turn the large FMS knob to highlight the ﬁeld of the Vspeed to be changed. 2.
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PRIMARY FLIGHT DISPLAY To view information about an airport: 1. Press the NRST softkey to display a list of the Nearest Airports. 2. Turn the FMS knob to select the desired airport and press the ENT key. The airport information is displayed with ‘BACK’ highlighted at the bottom of the window. 3. When ﬁnished viewing the airport information, press the ENT key to return to the nearest airports list. To activate a Direct-to from the Nearest Airports Window: 1.
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PRIMARY FLIGHT DISPLAY Direct-to Window NOTE: When entering an all-letter/alphabetical airport identiﬁer (only in the USA), the pilot must precede it with the letter “K” (e.g., KMCI). If the airport identiﬁer is alpha-numeric, simply enter the three-digit identiﬁer (e.g., 51K). The full ICAO identiﬁer must be entered for all waypoints. The Direct-to Window is enabled/disabled by pressing the Direct-to key. To select a Direct-to by identiﬁer: 1.
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PRIMARY FLIGHT DISPLAY To select a Direct-to from the Nearest Airports list: 1. Press the Direct-to key, then turn the large FMS knob to highlight the NRST ﬁeld. 2. Turn the small FMS knob to display a selection window showing the 25 nearest airports. 3. Turn the FMS knob to scroll through the list and highlight the desired airport, then press the ENT key. 4. Press the ENT key again to activate the direct-to.
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PRIMARY FLIGHT DISPLAY • • • • • • • • Activate Leg Activate leg selects the highlighted leg as the “active leg” (the ﬂight plan leg which is currently used for navigation guidance). Load Arrival Load Approach Remove Departure Remove Arrival Remove Approach Closest Point of FPL Change Fields Restore Defaults To activate a ﬂight plan along a speciﬁc leg: 1.
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PRIMARY FLIGHT DISPLAY To store a ﬂight plan: 1. From the Flight Plan Window, once all the waypoints have been entered, press the MENU key to display the page menu options. 2. Turn the FMS knob to select ‘Store Flight Plan’, then press the ENT key. The Store Flight Plan Window is displayed with ‘OK’ highlighted. 3. Press the ENT key to store the ﬂight plan. 4. To cancel, turn the large FMS knob to highlight ‘CANCEL’ and press the ENT key.
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PRIMARY FLIGHT DISPLAY Load Departure Load Departure allows the pilot to select a published standard instrument departure (SID) for the departure airport, or replace the current departure with a new selection. When using a direct-to, the G1000 uses the nearest airport as a reference when displaying available departures. Figure 2-58 Departure Runway NOTE: The PROC key can also be used to load a departure, an approach, or an arrival. To select a departure for the departure airport: 1.
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PRIMARY FLIGHT DISPLAY Load Arrival Load Arrival allows the pilot to select a published standard terminal arrival route (STAR) for the destination airport, or replace a current arrival with a new selection. NOTE: The PROC key can also be used to load a departure, an approach, or an arrival. NOTE: When adding an arrival to an active ﬂight plan, the pilot may need to remove a duplicate destination waypoint from the ﬂight plan list. To select an arrival for a direct-to or ﬂight plan destination airport: 1.
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PRIMARY FLIGHT DISPLAY Remove Departure, Arrival, or Approach Remove Departure, Arrival, or Approach deletes the current standard instrument departure (SID), terminal arrival route (STAR), or selected approach from the active ﬂight plan. To remove a departure, an arrival, or an approach from a direct-to or active ﬂight plan: 1. From the Flight Plan Window, press the MENU key to display the page menu options. 2.
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PRIMARY FLIGHT DISPLAY Procedures Window The Procedures Window is enabled and disabled by pressing the PROC key. The following options are available from the Procedures Window: Figure 2-62 Change Fields on Flight Plan To change a data ﬁeld on the Flight Plan Window: 1. 2. 3. 4. 5. From the Flight Plan Window, press the MENU key to display the page menu options. Turn the FMS knob to highlight ‘Change Fields’, then press the ENT key. The cursor ﬂashes on one of the data ﬁelds.
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PRIMARY FLIGHT DISPLAY Figure 2-64 Approach 3. Turn the FMS knob to select the desired approach, then press the ENT key. A window appears listing the available transitions for the approach. 5. With ‘LOAD?’ highlighted, press the ENT key to load the approach. 6. To activate the approach, turn the large FMS knob to highlight ‘ACTIVATE?’, then press the ENT key. NOTE: ‘LOAD’ adds the approach to the ﬂight plan without immediately using the approach for navigation guidance.
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PRIMARY FLIGHT DISPLAY 3. Turn the FMS knob to select the desired arrival, then press the ENT key. A window appears listing the available transitions for the arrival. NOTE: When adding an arrival to an active ﬂight plan, the pilot may need to remove a duplicate destination waypoint from the ﬂight plan list. Figure 2-68 Arrival Transition 4. 5. Turn the FMS knob to select the desired transition, then press the ENT key. A window may appear listing runways for the arrival.
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PRIMARY FLIGHT DISPLAY Activate Vector-To-Final NOTE: The runway window is not displayed for every departure. ‘ALL’ may appear in the runway ﬁeld, indicating that the departure procedure applies to all runways. For airports with parallel runways, ‘B’ may appear at the end of the runway designation to indicate that the departure procedure applies to both runways. 5. 6. Turn the FMS knob to select the desired transition, then press the ENT key. With ‘LOAD?’ highlighted, press the ENT key.
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PRIMARY FLIGHT DISPLAY 2.7 REVERSIONARY MODE NOTE: Refer to the System Overview for a detailed description of Reversionary mode. The PFD is designed to enter a reversionary (backup) mode based on automatic fault monitoring and detection internal switching. Reversionary mode can also be activated by manually pressing a dedicated DISPLAY BACKUP button at the bottom of the Audio Panel (refer to Audio Panel section).
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PRIMARY FLIGHT DISPLAY 2.8 ALERTS AND ANNUNCIATIONS NOTE: For a detailed description of all annunciations and alerts, refer to the Annunciations and Alerts section. Annunciation Window ANNUNCIATION WINDOW The Annunciation window appears to the right of the Vertical Speed Indicator when a WARNING or CAUTION alert is issued. Warning alerts are displayed in red and caution alerts are displayed in yellow.
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PRIMARY FLIGHT DISPLAY Caution indicates the existence of abnormal conditions on the aircraft that may require pilot intervention. A ﬂashing “CAUTION” softkey annunciation and a single aural tone (one chime) are used to alert the pilot of any cautions. The ﬂashing “CAUTION” annunciator continues to ﬂash until acknowledged by the pilot (by pressing the CAUTION softkey). NOTE: If a second TA appears or if the TAs displayed decrease and then increase, new aural and visual alerts are generated.
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PRIMARY FLIGHT DISPLAY This page intentionally left blank 2-46 Garmin G1000 Pilot’s Guide for the Diamond DA40 190-00592-00 Rev.
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G1000 TM NAV/COM
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Garmin G1000 Pilot’s Guide for the Diamond DA40 190-00592-00 Rev.
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NAV/COM 3.1 NAV/COM INTRODUCTION The NAV/COM frequency controls and windows are located in the top corners of the Primary Flight Display (PFD) and Multi Function Display (MFD). The NAV controls and NAV frequency window are located on the left side, the COM controls and COM frequency window are on the right. The ADF/DME Tuning window is located in the lower right corner on the PFD, as shown in the ﬁgure below.
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NAV/COM WINDOWS AND FIELDS RADIO SELECTION The NAV and COM Frequency windows are located at the top of the display on either side of the Navigation Status bar on both the PFD and the MFD. Frequencies in the active window are displayed in either green or white. • The NAV Frequency window is displayed to the left of the Navigation Status bar. • The COM Frequency window is displayed to the right of the Navigation Status bar.
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NAV/COM CONTROLS The COM controls: The NAV Frequency window is controlled by knobs and keys on the left, the COM Frequency window by knobs and keys on the right. • VOL/PUSH SQ knob – Turn to adjust the COM radio volume. – Press to turn automatic squelch ON and OFF. The NAV controls: • VOL/PUSH ID knob – Turn to adjust the NAV radio volume level. – Press to turn the Morse code ID ON and OFF. • Frequency Transfer key – Press to transfer the NAV frequencies between the active and standby ﬁelds.
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NAV/COM TUNING BOX A light blue tuning box is displayed around the radio standby frequency window, on both the PFD and MFD. Pressing the small COM or NAV knob transfers the tuning box back and forth between the two windows. Frequencies located in the standby window are displayed in either white or gray. Pushing the small COM knob switches the tuning box from one COM radio to the other. Figure 3-5 Switching COM Radios • The standby frequency appearing in the tuning box is white.
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NAV/COM RADIO INDICATORS • RX – During COM signal reception, a white RX appears by the active COM frequency. • TX – During COM transmission, a white TX appears by the active COM frequency replacing the Frequency Transfer Arrow. Figure 3-9 COM and NAV Volume Levels FREQUENCY TRANSFER ARROW Figure 3-7 COM Radio Status Indications • ID – When the Morse code identiﬁer is ON for a NAV radio, a white ID appears to the left of the active NAV frequency.
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NAV/COM 3.2 COM OPERATION FREQUENCY SPACING The G1000 COM radios can tune either 25 kHz spacing (118.000 to 136.975 MHz) or 8.33 kHz spacing (118.000 to 136.990 MHz) for 760-channel or 3040-channel conﬁguration. COM channel spacing is conﬁgured through the MFD on the System Setup Page of the AUX Page group. SELECTING A COM RADIO The desired COM radio is selected using the COM MIC keys on the audio panel.
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NAV/COM EMERGENCY FREQUENCY (121.500 MHZ) In case of a COM system tuning failure, the emergency frequency (121.500 MHz) is automatically tuned in the radio in which the tuning failure occurred. QUICK-TUNING AND ACTIVATING 121.500 MHZ Pressing and holding the COM Frequency Transfer key for two seconds automatically loads the emergency COM frequency (121.500 MHz) in the active ﬁeld of the active COM radio (the one with the transfer arrow).
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NAV/COM 3.3 NAV OPERATION NAV RADIO SELECTION FOR NAVIGATION The desired NAV radio is selected for navigation by pressing the CDI softkey located on the PFD. The three navigation modes that can be selected are: FREQUENCY RANGE The NAV radios receive in the VOR/ILS frequency range of 108.00 to 117.95 MHz with 50 kHz spacing.
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NAV/COM 3.4 OPTIONAL RADIOS OVERVIEW Optionally, the G1000 system can support up to two (2) remotely-mounted Becker RA 3502 ADF receivers and up to two (2) remotely-mounted Honeywell KN 63 DME transceivers. • The Becker RA 3502 ADF receiver operates in the 190.0 kHz to 1799.5 kHz frequency band with 0.5 kHz channel spacing. • The Honeywell KN 63 is a 200-channel, 100-watt, all-solid-state digital DME transceiver that provides distance information to the G1000 system.
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NAV/COM Tuning and Transferring ADF Frequencies NOTE: The active ADF frequency ﬁeld cannot be edited directly. ADF frequencies in the 190.0 kHz to 1799.5 kHz frequency range can be entered in the standby ADF frequency ﬁeld of the ADF/DME Tuning window, using both the dual FMS knob and the ENT key. NOTE: Pressing the CLR key while in data entry mode (i.e.
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NAV/COM Selecting the ADF Receiver Mode The following modes can be selected: • ANT (antenna) – The ADF bearing pointer is deﬂected on the HSI by approximately 90 degrees relative to the aircraft heading. In this mode, the NDB Morse code identiﬁer can only be heard if the ADF key is selected on the audio panel. • ADF – The ADF bearing pointer moves to point in the direction of the NDB station. In this mode, the NDB Morse code identiﬁer can only be heard if the ADF key is selected on the audio panel.
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NAV/COM Selecting the DME Transceiver Tuning Mode The following DME transceiver tuning modes can be selected: NOTE: Please refer to the Primary Flight Display section for information on the DME Information window. • NAV1 – Tunes the DME frequency from the selected NAV1 frequency. • NAV2 – Tunes the DME frequency from the selected NAV2 frequency. • HOLD – When transitioning from NAV1 or NAV2 mode to HOLD mode, the DME frequency remains set to the last selected NAV frequency.
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NAV/COM 3.5 FREQUENCY AUTO-TUNING The G1000 system offers multiple auto-tuning capabilities. The PFD allows auto-tuning of COM frequencies associated with the nearest airports. The MFD provides auto-tuning of both COM and NAV frequencies from waypoint and nearest pages. In addition, the primary NAV frequency is entered automatically in the NAV window during approach loading or approach activation.
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NAV/COM AUTO-TUNING ON THE MFD WPT – Airport Information Window Frequencies can be selected and loaded from the following MFD pages: The Airport Information Window displays runway information and a list of frequencies for the selected airport identiﬁer as well as departure, arrival, and approach information. • WPT – Airport Information • WPT – VOR Information To display the entire list of frequencies for an airport: • NRST – Nearest Airports • NRST – Nearest VOR 1.
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NAV/COM To load a COM frequency into the COM tuning box: To load the primary approach NAV frequency into the NAV tuning box: 1. When the list of frequencies for the selected airport is displayed, highlight the desired frequency by turning the large FMS knob. 1 On the Airport Information Window, press the APR softkey to display approach information for a speciﬁc airport. 2. Press the ENT key. 2. Press the FMS knob to activate the selection cursor in the window. 3.
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NAV/COM WPT – VOR Information Page The VOR Information Page displays information speciﬁc to individual VORs, including the airport that is nearest to the selected VOR. To load a VOR frequency into the NAV window: 1. On the VOR Information Page, press the FMS knob to activate the VOR Information window. 2. Turn the FMS knob as needed to select the desired VOR and press the ENT key to validate the selection. 3.
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NAV/COM NRST – Nearest Airports Page The Nearest Airports Page displays a list of the nearest airports as well as related runway, frequency and approach information. On this page, any frequency associated with the selected airport can be loaded into the NAV or COM Frequency window. To display the entire list of frequencies for a nearby airport and load a frequency from that list: 1. On the Nearest Airports Page, press the FMS knob to activate the selection cursor in the Nearest Airports window. 2.
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NAV/COM NRST – Nearest VOR Page The Nearest VOR Page displays a list of the nearest VORs together with related information, including the associated VOR frequency. To load a VOR frequency into the NAV window: 1. On the Nearest VOR Page, press the FMS knob to activate the Nearest VOR window. 2. Turn the FMS knob to scroll through the list of nearest VORs until the desired nearest VOR is highlighted. 3.
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NAV/COM NRST – Nearest Frequencies Page The Nearest Frequencies Page displays a list of nearest ARTCC, FSS and WX frequencies. For the purpose of frequency selection, the selection cursor can be activated on the ARTCC, FSS, or WX box by using the ARTCC, FSS, or WX softkeys, respectively. To view a nearest ARTCC frequency and load it into the standby frequency ﬁeld: 1. Press the ARTCC softkey to activate the selection cursor in the Nearest ARTCC box. 2.
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NAV/COM AUTO-TUNING UPON APPROACH ACTIVATION (NAV FREQUENCIES) NAV frequencies can be automatically loaded into the NAV Frequency window upon approach activation, regardless of the display unit being used. NOTE: The primary NAV frequency becomes auto-tuned upon loading of an approach. To auto-tune a NAV frequency if the desired approach is not already loaded: 1. Press the PROC key to open the Procedures window. 2.
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NAV/COM To auto-tune a NAV frequency if the desired approach is already loaded: 1. Press the PROC key to open the Procedures window. 2. Turn the large FMS knob to highlight the ‘ACTIVATE APPROACH’ menu option and press the ENT key. The approach primary NAV frequency becomes automatically loaded into the standby ﬁeld of the selected NAV radio.
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G1000 TM Transponder
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Garmin G1000 Pilot’s Guide for the Diamond DA40 190-00592-00 Rev.
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TRANSPONDER 4.1 TRANSPONDER DESCRIPTION The GTX 33 transponder is integrated into the G1000 system, offering Mode A, Mode C, and Mode S interrogation and reply capabilities. This section provides a description of transponder operation and information on Mode S capability. The transponder controls are located on the G1000 Primary Flight Display (PFD) on the lower portion of the screen (see ﬁgures below).
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TRANSPONDER MODE S FEATURES The GTX 33 transponder is equipped with selective addressing or Mode Select (Mode S), capability.
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TRANSPONDER 4.2 OPERATION MODE SELECTION Mode selection can be automatic (Ground and Altitude modes) or manual (Standby, ON and Altitude modes). The STBY, ON and ALT softkeys can be accessed by pressing the XPDR softkey. Standby Mode (Manual) The Standby mode can be selected at any time by pressing the STBY softkey. In Standby mode, the transponder does not reply to interrogations, but new codes can be entered.
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TRANSPONDER Altitude Mode (Automatic or Manual) CODE SELECTION Altitude mode is automatically selected when the aircraft becomes airborne. Altitude mode may also be selected manually by pressing the ALT softkey. Entering a Code If Altitude mode is selected, a green ALT indication is displayed in the mode ﬁeld of the Transponder Status bar, and all transponder replies requesting altitude information are provided with pressure altitude information.
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TRANSPONDER VFR Code IDENT FUNCTION The VFR code can be entered either manually, each digit at a time, or by pressing the XPDR softkey, then the VFR softkey. When the VFR softkey is pressed, the preprogrammed VFR code is automatically displayed in the code ﬁeld of the Transponder Status bar. Pressing the IDENT softkey sends an ID indication to Air Trafﬁc Control (ATC). The ID return distinguishes your transponder from all others on the air trafﬁc controller’s radar screen.
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G1000 TM Audio Panel
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Garmin G1000 Pilot’s Guide for the Diamond DA40 190-00592-00 Rev.
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AUDIO PANEL 5.1 AUDIO PANEL DESCRIPTION The GMA 1347 is an audio control panel and marker beacon system. Pressing the audio panel keys controls audio selection of COM, NAV, and intercom. LED annunciators indicate when a key function is selected. The audio panel includes a four-position intercom system (ICS) with electronic cabin noise de-emphasis. Separate knobs control intercom audio level for the pilot and copilot/passenger.
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AUDIO PANEL MONO/STEREO HEADSETS AUDIO PANEL CONTROLS Stereo headsets are recommended for use in this aircraft. Using a monaural headset in a stereo jack shorts the right headset channel output to ground. While this does not damage the audio panel, a person listening on a monaural headset hears only the left channel in both ears.
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AUDIO PANEL Transmitters Transceiver Audio Disabled on Diamond DA40 Aircraft Speaker Passenger Address Marker Beacon Signal Sensitivity Marker Beacon/Mute Navigation Radio Audio Navigation Radio Audio Disabled on Diamond DA40 Aircraft Manual Squelch Digital Recording Playback ICS Isolation VOL/SQ VOL Annunciation SQ Annunciation Reversionary Mode Control Figure 5-1 Audio Panel Controls 190-00592-00 Rev.
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AUDIO PANEL 5.2 OPERATION POWER-UP AND FAIL-SAFE OPERATION Power-up The audio panel performs a self-test during power-up. All panel annunciator lights illuminate for approximately two seconds. Once the self-test is completed, settings are restored to the ones in use before the unit was last turned off.
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AUDIO PANEL MARKER BEACON RECEIVER Transmitting NOTE: Audio level of the COM radio(s) is controlled by the COM volume controls located on both the PFD and MFD (see the NAV/COM section). When a transmitter is keyed, the active transceiver MIC key annunciator blinks approximately once per second. A white TX indication appears next to the active COM frequency on both the PFD and the MFD during transmission. PA FUNCTION A passenger address function is provided by pressing the PA key to deliver messages.
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AUDIO PANEL Marker Beacon Signal Sensitivity NAVIGATION RADIOS Press the HI SENS key (Figure 5-3) for increased marker beacon signal sensitivity. The HI SENS function is used to receive an earlier indication of nearing a marker during an approach. Pressing DME, ADF, NAV1, or NAV2 selects/deselects the radio source and the annunciator. Selected audio can be heard over the headset and the speakers. All radio keys can be selected individually or together.
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AUDIO PANEL INTERCOM SYSTEM (ICS) ISOLATION CREW Mode The intercom system (ICS) provides four isolation modes: ALL, PILOT, COPILOT, and CREW. The desired mode can be selected or deselected using the PILOT and COPLT keys. The four possible ICS isolation states are summarized in Table 5-2. CREW mode is selected when both the PILOT and COPLT key annunciators are lit.
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AUDIO PANEL INTERCOM VOLUME AND SQUELCH The MAN SQ key and VOL/SQ knob control the volume and squelch of the intercom. The MAN SQ key allows either automatic or manual control of the squelch setting. The VOL/SQ knob controls volume or manual squelch adjustment for the pilot and copilot/passenger. When the MAN SQ annunciator is not lit (auto-squelch is on), the VOL/SQ knob controls only the volume. When the MAN SQ annunciator is lit (manual squelch), the VOL/SQ knob controls both volume and squelch.
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AUDIO PANEL DIGITAL CLEARANCE RECORDER WITH PLAYBACK CAPABILITY The audio panel contains a digital clearance recorder that plays back up to 2.5 minutes of COM signal recording. Recorded COM audio is stored in separate memory blocks. Audio from all of the selected COM radios are recorded and can be played back. Anyone able to hear the selected COM radios is able to hear the COM audio playback. Once the 2.
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ENGINE INDICATION SYSTEM 6.1 INTRODUCTION The G1000 Engine Indication System (EIS) provides the ﬂight crew with gauges, bar graphs, and numeric readouts of engine parameters. The EIS is displayed on the left side of the MFD during normal operations. In reversionary mode, the GDUs are re-conﬁgured to present PFD symbology together with the EIS (the EIS is displayed on the left side). NOTE: Refer to the System Overview for information regarding reversionary mode.
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ENGINE INDICATION SYSTEM 6.2 DA40 & DA40F ENGINE PAGE Beneath the gauges are horizontal bar indicators for fuel ﬂow, cylinder head temperature (CHT), oil temperature, oil pressure, alternator amperage, bus voltage and fuel quantity. The CHT (Cylinder Head Temperature) indicator displays the temperature of the hottest cylinder in degrees Fahrenheit. The number of the hottest cylinder appears in the triangular pointer.
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ENGINE INDICATION SYSTEM Fuel Qty GAL Indicator The Fuel Quantity indicator displays the quantity of fuel in the tanks, in gallons. Two (2) triangular pointers labeled L (left) and R (right) indicate the number of gallons in each fuel tank. Manifold Pressure Gauge • Green – Normal • Yellow – Caution • Red – Warning Tachometer Standard Tanks The indicator ranges from 0 to 20 with tick marks at 5, 10, and 15 gallons. The Fuel Quantity Indicator only displays to 17 gallons per side when full.
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ENGINE INDICATION SYSTEM LEAN PAGE The Lean Page is accessed by pressing the LEAN softkey. A digital readout for fuel ﬂow resides below the tachometer. Beneath the fuel ﬂow indication are bar graphs and numeric readouts for exhaust gas temperature (EGT), temperature deviation from peak and cylinder head temperature (CHT) in degrees Fahrenheit. By default, the numeric readouts of the EGT and CHT are associated with the hottest cylinder and are graphically indicated in cyan (light blue).
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ENGINE INDICATION SYSTEM Manifold Pressure Gauge Tachometer Fuel Flow Indicator Hollow Bar Representing Peak Exhaust Gas Temperature Bar Graph (with readout for selected cylinder) Temperature Deviation from Peak Cylinder Head Temperature Bar Graph (with readout for selected cylinder) DA40 DA40F Figure 6-3 Lean Page 190-00592-00 Rev.
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ENGINE INDICATION SYSTEM SYSTEM PAGE The System Page is accessed by pressing the SYSTEM softkey. The readouts on this page are separated into two categories: System and Fuel Calculation. The System readouts include oil temperature and pressure, voltage, amperes, fuel ﬂow, and optional fuel pressure (DA40 only; see Figure 6-4).
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ENGINE INDICATION SYSTEM Manifold Pressure Gauge Tachometer Oil Temperature Oil Pressure Voltmeter Ammeter Fuel Flow Oil Temperature Oil Pressure Voltmeter Ammeter Fuel Flow Fuel Remaining Fuel Used Endurance Range Fuel Remaining Fuel Used Endurance Range Total Time in Service DA40F DA40 Figure 6-5 System Page 190-00592-00 Rev.
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ENGINE INDICATION SYSTEM 6.3 DA40D The Fuel Flow indicator is a digital readout which displays current fuel ﬂow in gallons per hour (GPH) and has no color bands. ENGINE PAGE Atop all three pages are two round dial gauges for engine load and revolutions per minute (RPM). Beneath those gauges is a digital readout for fuel ﬂow. Below the fuel ﬂow readout are horizontal bar indicators for oil temperature, oil pressure, coolant temperature, fuel temperature and fuel quantity.
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ENGINE INDICATION SYSTEM Fuel Quantity Indicator The Fuel Quantity indicator displays the quantity of fuel in the tanks, in gallons. The indicator ranges from 0 to 15 with tick marks at 0, 5, 10 and 15 gallons. • Green – Normal • Red – Warning Engine Load Indicator NOTE: The Fuel Quantity Indicator displays 14 gallons per side when full. NOTE: Pilots should refer to the Aircraft Flight Manual Supplement (AFMS) for limitations.
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ENGINE INDICATION SYSTEM SYSTEM PAGE The System Page is accessible by pressing the SYSTEM softkey. The indications for this page are separated into three categories: Electrical, Engine and Oil. Beneath the tachometer are horizontal bar indicators for the voltmeter, ammeter and gearbox temperature, followed by a digital readout for coolant temperature, oil temperature and oil pressure.
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ENGINE INDICATION SYSTEM FUEL PAGE The Fuel Page is accessible by pressing the FUEL softkey. All readouts for this page are digital and are separated into two categories: Fuel and Fuel Calculations. Beneath the tachometer are readouts for the fuel ﬂow, fuel quantity and fuel temperature. The fuel calculation portion of the Fuel Page is based on the fuel ﬂow totalizer and displays the following: • GAL REM – Current fuel remaining in gallons as set by the pilot and adjusted for fuel burn since last set.
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MULTI FUNCTION DISPLAY 7.1 INTRODUCTION MFD POWER-UP This section of the Pilot’s Guide describes the Multi Function Display (MFD) as installed in Diamond DA40, DA40F, and DA40D aircraft. DESCRIPTION The display portion of the G1000 Integrated Cockpit System consists of two 10.4-inch liquid crystal displays (LCDs). During normal operation, the right display is conﬁgured as the Multi Function Display (MFD).
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MULTI FUNCTION DISPLAY MFD SOFTKEYS MAP – Enables the following softkeys: TRAFFIC – Displays/removes Mode S Trafﬁc on the Navigation Map TOPO – Displays/removes topographic information on the Navigation Map TERRAIN – Displays/removes terrain information on the Navigation Map BACK – Displays the ENGINE and MAP top level softkeys DCLTR (declutter) – Removes map information in three levels CHKLIST (checklist) – Displays the Checklist Page The MFD softkeys are located below the display screen and provide con
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MULTI FUNCTION DISPLAY ELECTRONIC CHECKLISTS (OPTIONAL) The G1000 Multi Function Display provides optional checklists which allow a pilot to quickly ﬁnd the proper procedure on the ground and during each phase of ﬂight. NOTE: The checklist information described in this section is not intended to replace the checklist information described in the Diamond Information Manual and the Pilot Safety and Warning Supplements document. NOTE: Garmin is not responsible for the content of the checklists.
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MULTI FUNCTION DISPLAY Removing the Check mark from a Checklist Item Press the CLR key to remove a check mark from an item. Advancing to the Next Checklist Once the last item in a checklist is selected, the ‘GO TO THE NEXT CHECKLIST?’ text is highlighted. Press the ENT key to advance to the next checklist displayed. One-Button Access to Emergency Procedures The EMERGENCY softkey is available at all times when the checklist page is displayed.
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MULTI FUNCTION DISPLAY MFD PAGE GROUPS To select a speciﬁc page group: The MFD displays GPS/Navigation ﬂight information in four main page groups: • Map (MAP): Navigation Map Page Trafﬁc Map Page Terrain Proximity Page • Waypoint (WPT) : Airport Information Page Intersection Information Page NDB Information Page VOR Information Page User Waypoint Information Page • Auxiliary (AUX): Trip Planning Page Utility Page GPS Status Page System Setup Page System Status Page • Nearest (NRST): Nearest Airports Page
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MULTI FUNCTION DISPLAY WORKING WITH MENUS Much of the operation of the G1000 MFD is accomplished using a menu interface. The G1000 has a bezel-mounted dedicated menu key (MENU) when pressed, displays a context-sensitive list of options. This options list allows the pilot to access additional features or make settings changes which speciﬁcally relate to the currently displayed page. Some menus provide access to additional submenus that are used to view, edit, select, and review options.
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MULTI FUNCTION DISPLAY 7.2 NAVIGATION MAP PAGE WARNING: Use of the Navigation Map Page for pilotage navigation is prohibited. The Navigation Map is intended only to enhance situational awareness. Navigation is to be conducted using only current charts, data, and authorized navigation facilities.
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MULTI FUNCTION DISPLAY To select the Navigation Map Page: 1. Turn the large FMS knob to select the Map Page group. 2. Turn the small FMS knob to select the Navigation Map Page. The page group name and page title is displayed below the navigation status bar; MAP – NAVIGATION MAP. In addition to turning the large and small FMS knobs, the Navigation Map Page can be selected from any page by pressing and momentarily holding the CLR (DFLT MAP) key.
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MULTI FUNCTION DISPLAY Identifying Aviation Map Data The following aviation data is displayed on the Navigation Map Page: Airport Symbols: • Non-towered airports (purple in color). • Towered airports (blue in color). • Non-serviced airports (displayed as solid circle icons). See Appendix F for symbology deﬁnitions. • Serviced airports (displayed as circles with protruding tick marks pointing to the top, bottom, left, and right portions of the screen).
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MULTI FUNCTION DISPLAY Decluttering the Map The Navigation Map Page can be quickly decluttered by repeatedly pressing the DCLTR softkey until the desired detail is displayed. The declutter level label is displayed above the DCLTR softkey. Note that during an instrument approach, automatic decluttering takes place. Table 71 lists the features that are turned off at each declutter level.
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MULTI FUNCTION DISPLAY Map Panning To pan the map: Map panning moves the map beyond its current limits without adjusting the map range. When the panning function is selected by pushing in the joystick, a panning arrow ﬂashes on the map display. A window also appears at the top of the map display showing the latitude/longitude position of the pointer, the bearing and distance to the pointer from the aircraft’s present position, and the elevation of the land at the position of the pointer.
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MULTI FUNCTION DISPLAY Displaying Topographic Data on the Navigation Map Page The Navigation Map Page displays various shades of topography land colors representing the rise and fall of land elevation similar to aviation sectional charts. The Navigation Map Page can display a topographic scale representing various key points of terrain elevation colors with their associated elevation value labeled. Maximum NOTE: Press the TOPO softkey again to remove topo data from the Navigation Map Page.
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MULTI FUNCTION DISPLAY Displaying Trafﬁc on the Navigation Map Page MFD Data Bar Pressing the TRAFFIC softkey displays Trafﬁc Information Service (TIS) trafﬁc on the Navigation Map Page. TIS is a ground-based service providing relative location of all ATCRBS Mode-A and Mode-C transponder equipped aircraft within a speciﬁed service volume. The TIS ground sensor uses real time track reports to generate trafﬁc notiﬁcation.
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MULTI FUNCTION DISPLAY Map Setup Orientation The ﬁrst option is ‘Map Setup’ which is used to conﬁgure the Navigation Map Page including map orientation, land data enable/disable, Jeppesen data enable/disable, automatic zoom, airspace boundaries, and text size. Map Group Options There are four map orientation selections: North up, Track up, DTK up, and HDG up. • North up ﬁxes the top of the map to a north heading. • Track up adjusts the top of the map display to the current ground track.
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MULTI FUNCTION DISPLAY Auto Zoom Land Data The automatic zoom feature automatically adjusts the map range from 2000 nm through each lower range, stopping at 1.5 nm as the aircraft approaches the destination waypoint. To enable/disable automatic zoom: The Navigation Map Page can display background land data (roads, lakes, borders, etc). The background land data can also be removed from the display (turned off). To enable/disable land data: 1.
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MULTI FUNCTION DISPLAY Track Vector Wind Vector The Navigation Map Page can display a track vector as a dashed cyan line segment with an arrowhead attached to the end, extended to a predicted location in 60 seconds along the current aircraft track. The track vector is useful in minimizing track angle error. To enable/disable the track vector: To enable/disable the wind vector box: 1. 1. With the Navigation Map Page displayed, press the MENU key to display the Navigation Map Page Menu.
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MULTI FUNCTION DISPLAY Nav Range Ring Topo Data The Nav range ring shows the direction of travel (ground track) on a rotating compass card. The range of the Nav compass is determined by the map range, 125 feet (500 feet map range) to 500 nm (2000 nm map range). To enable/disable the Nav range ring: 1. 2. 3. 4. 5. 6. With the Navigation Map Page displayed, press the MENU key to display the Navigation Map Page Menu. The cursor ﬂashes on the ‘Map Setup’ option.
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MULTI FUNCTION DISPLAY Topo Range Terrain Data The topo range setting enables or disables the topography range box located in the lower right corner of the Navigation Map Page. To enable/disable the topo range box: 1. 7-18 With the Navigation Map Page displayed, press the MENU key to display the Navigation Map Page Menu. The cursor ﬂashes on the ‘Map Setup’ option. Terrain data can be enabled or disabled on the Navigation Map Page using the ‘TERRAIN DATA’ setting. A data range can also be selected.
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MULTI FUNCTION DISPLAY Obstacle Data Fuel Range Ring (Fuel RNG) (RSV) Obstacle data can be enabled or disabled on the Navigation Map Page using the ‘OBSTACLE DATA’ setting. A data range can also be selected. The data range is the maximum map range that terrain data is displayed. To enable/disable obstacle data and to select a terrain data range: 1. With the Navigation Map Page displayed, press the MENU key to display the Navigation Map Page Menu. The cursor ﬂashes on the ‘Map Setup’ option.
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MULTI FUNCTION DISPLAY Trafﬁc Group The display of trafﬁc information on the Navigation Map Page closely resembles TCAS display symbology. Trafﬁc is only displayed on the Navigation Map Page if aircraft heading data is available. If heading is not available, trafﬁc advisories are displayed as non-bearing banners on the Navigation Map Page. To enable/disable trafﬁc data on the Navigation Map Page: 1. With the Navigation Map Page displayed, press the MENU key to display the Navigation Map Page Menu.
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MULTI FUNCTION DISPLAY To select a trafﬁc mode: To select a trafﬁc symbol zoom range: 1. With the Navigation Map Page displayed, press the MENU key to display the Navigation Map Page Menu. The cursor ﬂashes on the ‘Map Setup’ option. 1. With the Navigation Map Page displayed, press the MENU key to display the Navigation Map Page Menu. The cursor ﬂashes on the ‘Map Setup’ option. 2. Press the ENT key. The Map Setup Menu is displayed. 2. Press the ENT key. The Map Setup Menu is displayed 3.
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MULTI FUNCTION DISPLAY The trafﬁc label displays the altitude separation above or below the symbol and the vertical speed sense arrow to the right of the symbol. To select a trafﬁc label zoom range: 1. With the Navigation Map Page displayed, press the MENU key to display the Navigation Map Page Menu. The cursor ﬂashes on the ‘Map Setup’ option. 2. Press the ENT key. The Map Setup Menu is displayed 3. Turn the small FMS knob to select the ‘Trafﬁc’ group. Press the ENT key.
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MULTI FUNCTION DISPLAY • Airspace Boundaries (CLASS B/TMA, CLASS C/TCA, and CLASS D) - The airspace zoom range sets the maximum range at which the three classes of airspace appear on the display.
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MULTI FUNCTION DISPLAY To select an aviation group item text size: Land Group Options 1. With the Navigation Map Page displayed, press the MENU key to display the Navigation Map Page Menu. The cursor ﬂashes on the ‘Map Setup’ option. 2. Press the ENT key. The Map Setup Menu is displayed. • Latitude/Longitude (LAT/LON) - the LAT/LON label size sets the size at which latitude/longitude labels appear on the display (none, small, medium, and large).
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MULTI FUNCTION DISPLAY To select a land group item text size: Figure 7-16 Land Group Options To select a land group item range: 1. With the Navigation Map Page displayed, press the MENU key to display the Navigation Map Page Menu. The cursor ﬂashes on the ‘Map Setup’ option. 2. Press the ENT key. The Map Setup Menu is displayed. 3. Turn the small FMS knob to select the ‘Land’ group. Press the ENT key. The cursor ﬂashes on the ‘LAT/LON’ ﬁeld. 4. Turn the large FMS knob to select the desired option.
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MULTI FUNCTION DISPLAY Measure Bearing/Distance The second map setup option is ‘Measure Bearing/ Distance’ which provides a quick and easy method for determining the bearing and distance between any two points on the Navigation Map Page. NOTE: Pressing the ENT key at any location with the ‘Measure’ option enabled allows bearing and distance from the newly selected position to be acquired. To measure bearing and distance between two points: 1. Press the MENU key (with the Navigation Map Page displayed).
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MULTI FUNCTION DISPLAY 7.3 TRAFFIC MAP PAGE The Trafﬁc Map Page is the second page in the Map Group and displays the following information: • Current aircraft location, surrounding Trafﬁc Information System (TIS) trafﬁc, and range marking rings. • The current trafﬁc mode (OPERATE, STANDBY).
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MULTI FUNCTION DISPLAY TRAFFIC MAP PAGE OPERATIONS TIS SYMBOLOGY TIS trafﬁc is displayed on the Trafﬁc Map Page according to TCAS symbology. A Trafﬁc Advisory (TA) symbol is displayed as a solid yellow circle (or half circle on the outer range ring if the trafﬁc is outside the range of the dedicated trafﬁc page). All other trafﬁc is displayed as a hollow white diamond.
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MULTI FUNCTION DISPLAY Operating Mode To switch between operating modes: Once the aircraft is airborne (determined by system conﬁguration at the time of installation) the system switches from standby mode to operating mode. The G1000 displays ‘OPERATE’ in the upper left hand corner of the display and begins to display trafﬁc on the Trafﬁc or Map Page. The TIS Trafﬁc Advisory (TA) should alert the crew to use additional vigilance to identify the intruding aircraft.
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MULTI FUNCTION DISPLAY TIS Audio Alert TIS Trafﬁc Status A TIS audio alert is generated whenever the number of TAs on the Trafﬁc Map Page display increases from one scan to the next. The limiting to TAs only reduces the amount of “nuisance” alerting due to proximate aircraft. For example, when the ﬁrst TA is displayed, the pilot is alerted audibly. So long as a single TA aircraft remains on the TIS display, no further audio alert is generated.
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MULTI FUNCTION DISPLAY 7.4 TERRAIN PROXIMITY PAGE CAUTION: Use of Terrain Proximity information for primary terrain avoidance is prohibited. The Terrain Proximity Map is intended only to enhance situational awareness. It is the pilot’s responsibility to provide terrain avoidance at all times.
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MULTI FUNCTION DISPLAY TERRAIN PROXIMITY PAGE OPERATIONS There are two terrain/obstacle viewing options available (relative to the position of the aircraft), a radar-like ARC (120°) display and a 360° default display. To change the map range on the Terrain Proximity Page: To change the viewing mode between 360° and ARC: 1. Select the Terrain Proximity Page 2. Press the VIEW softkey. Press the ARC softkey. 3. To return to the 360 degree viewing display press the 360 softkey OR: 4.
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MULTI FUNCTION DISPLAY DISPLAYING OBSTACLE DATA The Terrain Proximity Page displays obstacle data with heights greater than 200 feet Above Ground Level (AGL) located at their geographical position location throughout the world. Obstacles are displayed in three levels. The G1000 will adjust colors on the Terrain Proximity Page automatically as the aircraft altitude changes.
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MULTI FUNCTION DISPLAY 7.5 DIRECT-TO NAVIGATION The “Direct-to” function provides a quick method of setting a course to a destination waypoint. Once a Direct-to is activated, the G1000 establishes a point-topoint course line from the present position to the selected Direct-to destination. If the course change is greater than 30 degrees, a course extension is offset from the present position to allow a standard rate turn to intercept the Direct-to course line.
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MULTI FUNCTION DISPLAY DIRECT-TO NAVIGATION OPERATIONS To select a Direct-to destination by facility name or city: Selecting a Direct-to Waypoint 1. Press the Direct-to key. The Direct-to Page is displayed with the waypoint identiﬁer ﬁeld highlighted. 2. Turn the large FMS knob to highlight the facility or city name ﬁeld. 3. Turn the small and large FMS knob to enter the facility or city location of the desired waypoint.
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MULTI FUNCTION DISPLAY Selecting a Direct-to Destination from the Active Flight Plan Any waypoint contained in the ﬂight plan may be selected as a Direct-to destination from the Direct-to Waypoint Page when navigating an active ﬂight plan. To select a Direct-to destination from the active ﬂight plan: 1. Press the Direct-to key. The Direct-to Waypoint Page is displayed with the waypoint identiﬁer ﬁeld highlighted. 2. Turn the large FMS knob to highlight the ﬂight plan ‘FPL’ ﬁeld. 3.
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MULTI FUNCTION DISPLAY Selecting the Nearest Airport as a Direct-to Destination The Direct-to Page always displays the nearest airports (from the present position) on the NRST ﬁeld. To select a nearby airport as a Direct-to destination: 1. Press the Direct-to key. The Direct-to Page is displayed with the destination ﬁeld highlighted. 2. Turn the large FMS knob to highlight the nearest airport ﬁeld. 3. Turn the small FMS knob to display a window showing up to nine nearby airports. 4.
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MULTI FUNCTION DISPLAY Canceling Direct-to Navigation Specifying a Course to a Waypoint Once a Direct-to is activated, the G1000 provides navigation guidance to the selected destination until the Direct-to is either replaced with a new Direct-to or ﬂight plan, or cancelled, or if the unit is turned off. During a Direct-to, the G1000 sets a direct great circle course to the selected destination. The course to the destination, using the course ﬁeld on the Direct-to Page can be manually deﬁned.
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MULTI FUNCTION DISPLAY 7.6 FLIGHT PLANS The G1000 can create up to 99 different ﬂight plans with up to 31 waypoints in each ﬂight plan.
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MULTI FUNCTION DISPLAY ACTIVE FLIGHT PLAN PAGE OPTIONS The following options are available for the Flight Plan Page: • • • • • • • • • • • • • Activate Leg Store Flight Plan Invert Flight Plan Delete Flight Plan Load Departure Load Arrival Load Approach Remove Arrival Remove Departure Remove Approach Closest Point of FPL Change Fields Restore Defaults Create a New Flight Plan ‘Create New Flight Plan’ creates a new ﬂight plan. To create a new ﬂight plan: 1.
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MULTI FUNCTION DISPLAY Activate Leg To edit a ﬂight plan: 1. Press the FPL key and turn the small FMS knob to display the Flight Plan Catalog Page. 2. Press the FMS knob to activate the cursor. 3. Turn the large FMS knob to highlight the desired ﬂight plan and press the ENT key. To activate a ﬂight plan along a speciﬁc leg: 4. To add a waypoint to the ﬂight plan: Turn the large FMS knob to select the point where the new waypoint is to be added.
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MULTI FUNCTION DISPLAY Store Flight Plan To store an existing ﬂight plan: Whenever an approach, departure or arrival is loaded into the active ﬂight plan, a set of approach, departure or arrival waypoints is inserted into the ﬂight plan along with a header line describing the instrument procedure the pilot selected. The original enroute portion of the ﬂight plan remains active (unless an instrument procedure is activated) which may be done when the procedure is loaded or at a later time.
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MULTI FUNCTION DISPLAY Invert Flight Plan Delete a Waypoint ‘Invert Fight Plan’ reverses the active ﬂight plan. After traveling along a ﬂight plan, the route can be reversed for navigation guidance back to the original departure point. To invert and (activate) an existing ﬂight plan: 1. From the Flight Plan Page, press the FMS knob to activate the cursor. 2. Turn the large FMS knob to highlight the desired ﬂight plan and press the MENU key to display the Flight Plan Page options. 3.
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MULTI FUNCTION DISPLAY Load a Departure ‘Load Departure’ allows a published departure procedure for the departure airport to be loaded into a ﬂight plan. It also replaces the current departure with a new selection. When using a Direct-to, the G1000 uses the nearest airport as a reference when displaying available departures. A departure can also loaded using the PROC key or by pressing the LD DP softkey. To select a departure procedure for the departure airport: 1.
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MULTI FUNCTION DISPLAY Load an Arrival ‘Load Arrival’ allows a published standard terminal arrival route (STAR) for the destination airport to be loaded into a ﬂight plan. It also replaces the current arrival with a new selection. An arrival can also be loaded using the PROC key or by pressing the LD STAR softkey. To select an arrival for a Direct-to or ﬂight plan destination airport: 1. From the Active Flight Plan Page, press the MENU key to display the Active Flight Plan Page options. 2.
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MULTI FUNCTION DISPLAY Load an Approach ‘Load Approach’ allows for the selection of a published instrument approach for the destination airport. It also replaces the current approach with a new selection. In many cases, it is more convenient to select approaches using the PROC key, or by pressing the LD APR softkey. This allows for the original ﬂight plan to continue navigating until cleared for the approach, but keeps the approach available for quick activation when needed.
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MULTI FUNCTION DISPLAY Remove a Departure, Arrival, or Approach • ‘Remove Departure’ deletes the current DP from the active ﬂight plan. • ‘Remove Arrival’ deletes the current STAR from the active ﬂight plan. • ‘Remove Approach’ deletes the currently selected approach from the active ﬂight plan.
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MULTI FUNCTION DISPLAY Change Fields Shortcuts ‘Change Fields’ allows for the default ﬁelds of DTK (distance) and DIS (distance) to be changed to one of the following: A number of shortcuts are available to save time when using the Active Flight Plan Page. These shortcuts speed the process of removing approaches, departures and arrivals, and aid in selecting a speciﬁc ﬂight plan leg for navigation guidance. On the preceding page, options to remove approaches, departures and arrivals were introduced.
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MULTI FUNCTION DISPLAY FLIGHT PLAN CATALOG PAGE FLIGHT PLAN CATALOG PAGE OPERATIONS The Flight Plan Catalog Page is the second ﬂight planning page and provides ﬂight planning information and editing capability.
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MULTI FUNCTION DISPLAY Activate a Flight Plan Stop Navigating a Flight Plan Once a ﬂight plan is deﬁned using the Flight Plan Catalog Page it can be activated for navigation. Activating the ﬂight plan overwrites any previous information at that location. To activate (begin to navigate) an existing ﬂight plan: 1. Press the FPL key and turn the small FMS knob to display the Flight Plan Catalog Page. 2. Press the FMS knob to activate the cursor. 3.
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MULTI FUNCTION DISPLAY Invert and Activate a Flight Plan ‘Invert & Activate FPL’ allows the active ﬂight plan to be inverted and activated for navigation. To invert and activate a ﬂight plan: 1. Press the FPL key and turn the small FMS knob to display the Flight Plan Catalog Page. 2. Press the FMS knob to activate the cursor. 3. Turn the large FMS knob to highlight the desired ﬂight plan and press the MENU key to display the Flight Plan Catalog Page options. 4.
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MULTI FUNCTION DISPLAY Copy a Flight Plan Delete a Flight Plan ‘Copy Flight Plan’ copies the active ﬂight plan to a Flight Plan Catalog location. The copy function is useful for duplicating the active ﬂight plan before making changes. ‘Delete Flight Plan’ removes all waypoints from the active ﬂight plan. (Deleting a ﬂight plan does not delete the waypoints contained in the ﬂight plan from the database or user waypoint memory.
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MULTI FUNCTION DISPLAY Delete All Flight Plans 3. ‘Delete All’ removes all ﬂight plans from memory at one time. To delete all ﬂight plans: 1. 2. From the Flight Plan Catalog Page, press the MENU key to display the Flight Plan Catalog Page options. Turn the large FMS knob to highlight ‘Delete All’ and press the ENT key. A ‘Delete all ﬂight plans?’ confirmation window is displayed. With ‘OK’ highlighted, press the ENT key to delete all ﬂight plans.
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MULTI FUNCTION DISPLAY Point-n-Shoot Flight Plan Creation Feature 4. If the selected waypoint is not a Jeppesen waypoint (Airport or Navaid) or user waypoint, the G1000 creates a user waypoint (beginning with ‘USR000’) at the point and inserts it into the ﬂight plan. 5. The pilot can also create and insert a user waypoint by pointing at a blank spot on the nav map and pressing ‘LD WPT’. This creates a user waypoint at the map cursor and inserts it into the ﬂight plan.
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MULTI FUNCTION DISPLAY VERTICAL NAVIGATION (VNAV) PAGE The Vertical Navigation Page allows the creation of a three-dimensional proﬁle which guides the aircraft from it’s present position and altitude to a ﬁnal (target) altitude at a speciﬁed location. This is helpful when you like to descend to a certain altitude near an airport or climb to an altitude before reaching a route or Direct-to waypoint.
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MULTI FUNCTION DISPLAY 7-56 3. With the ‘TARGET ALTITUDE’ ﬁeld highlighted, turn the small and large FMS knobs to select the target altitude and press the ENT key. With the proﬁle set, the vertical speed required (VSR) is displayed. Expect the following to occur when using the vertical navigation feature: 4. Turn the small FMS knob to select ‘Above Wpt’ (AGL) or ‘MSL’, and press the ENT key. ‘Above Wpt’ uses the altitude of a destination airport.
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MULTI FUNCTION DISPLAY 7.7 PROCEDURES To select a departure: 1. Press the PROC key to display the Procedures Page. Turn the large FMS knob to highlight ‘Select Departure’ and press the ENT key. 2. The ‘Departure Loading’ page is displayed with the list of departure options for the departure airport. Turn either the small or large FMS knobs to enter the desired departure. Press the ENT key. 3. ‘Load?’ is highlighted. Press the ENT key. The departure becomes part of the ﬂight plan.
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MULTI FUNCTION DISPLAY APPROACHES The G1000 allows you to ﬂy non-precision and precision approaches to airports with published instrument approach procedures. All available approaches are part of the Jeppesen database stored internally in each PFD and MFD. The G1000 provides both lateral and vertical guidance for ILS precision approaches on the PFD, and lateral guidance for non-precision Localizer, GPS, and VOR and ADF overlay approaches.
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MULTI FUNCTION DISPLAY SELECTING APPROACHES In order to select an approach, there must be an active ﬂight plan or direct-to which terminates at an airport with a published approach. To select an approach: 1. Press the PROC key to display the Procedures Page. Turn the large FMS knob to highlight ‘Select Approach’ and press the ENT key. The approach procedure window appears. 2. Turn the FMS knob to select the desired approach and press the ENT key. The transition window appears.
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MULTI FUNCTION DISPLAY Not all approaches in the database are approved for GPS use. As you select an approach, a ‘GPS’ designation to the right of the procedure name indicates the procedure can be ﬂown using the GPS receiver. Some procedures will not have this designation, meaning the GPS receiver can be used for supplemental navigation guidance only. If the GPS receiver cannot be used for primary guidance, you must use the appropriate receiver for the selected approach (e.g., VOR or ILS).
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MULTI FUNCTION DISPLAY 7.8 WAYPOINT PAGE GROUP The Waypoint Page Group (WPT) provides information for the thousands of airports, VORs, NDBs, intersections, runways, frequencies and procedures stored on the SD card. In addition, a user waypoint information page displays information for up to 1,000 user-created waypoints.
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MULTI FUNCTION DISPLAY AIRPORT INFORMATION PAGE (INFO) The Airport Information Page shows the following detailed information for the selected airport: • Airport Information • Runways • Frequencies Airport Information Page Operations To enter a waypoint identiﬁer: 7-62 Airports may be selected by identiﬁer, facility name or city location. To enter a waypoint facility name or city location: 1. Select the Airport Information Page. 2. Press the FMS knob to activate the cursor. 3.
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MULTI FUNCTION DISPLAY To select a facility name or city location, where duplicate entries exist: Facility Field Location Field 1. Select the desired facility name or location. 2. As you spell the facility name or location, using the small and large FMS knobs, the SpellNFind feature selects the ﬁrst entry in the database based upon the characters you have entered up to that point. 3.
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MULTI FUNCTION DISPLAY Airport Runway Information Field The Airport Runway Information ﬁeld displays runway designations, length, surface type and lighting for the selected airport. A map image of the runway layout and surrounding area is also displayed on the Airport Runway Information Page. The map image range is displayed in the lower left corner and is adjustable using the joystick. For airports with multiple runways, information for each runway is available.
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MULTI FUNCTION DISPLAY AIRPORT FREQUENCY INFORMATION FIELD The Airport Frequency Information Field displays radio frequencies and frequency types for the selected airport, as well as sector and altitude restrictions (where applicable). If the selected airport has a localizer-based approach, the localizer frequency is also listed on the Airport Frequency Information Field. The Airport Frequency Information Field may be used to quickly select and tune a COM or NAV frequency.
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MULTI FUNCTION DISPLAY Airport Frequency Descriptions AIRPORT INFORMATION PAGE OPTIONS The Airport Frequency Information ﬁeld uses the following descriptions and abbreviations: The following Airport Information Page options are available by pressing the MENU key (with the Airport Information Page displayed): • Frequency – Communication frequencies which may include restrictions: • Approach • Arrival • Class B • Class C • CAT • Departure • TMA • Terminal • TRSA Communication frequencies without restrict
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MULTI FUNCTION DISPLAY DEPARTURE INFORMATION PAGE (DP) The Departure Information Page shows the available Departure Procedures (DPs; also referred to as SIDs) for the selected airport. Where multiple runways or transitions are associated with the departure procedure, that information can also be displayed. A map image provides a layout diagram for each departure, runway and transition. To display the Departure Information Page press the DP softkey.
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MULTI FUNCTION DISPLAY ARRIVAL INFORMATION PAGE (STAR) The Arrival Information Page shows the available Standard Terminal Arrival (STAR) procedures for the selected airport. Where multiple transitions or runways are associated with the arrival procedure, that information may also be displayed. A map image provides a layout diagram for each arrival, transition and runway. To display the Airport Arrival Information Page press the STAR softkey.
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MULTI FUNCTION DISPLAY An arrival can be loaded from the Arrival Information Page. To load an arrival procedure from the Arrival Information Page: APPROACH INFORMATION PAGE The Approach Information page shows the available approach procedures for a selected airport. Where multiple initial approach ﬁxes (IAFs) and feeder routes are available, that information may also be displayed. A map image provides a layout diagram for each approach and transition.
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MULTI FUNCTION DISPLAY NOTE: Not all approaches in the database are approved for GPS use. As you select an approach, a GPS designation to the right of the procedure name indicates the procedure can be ﬂown using the GPS receiver. Some procedures do not have this designation, meaning the GPS receiver may be used for supplemental navigation guidance only. VOR approaches, for example, must be ﬂown by tuning the NAV receiver to the proper frequency and coupling the NAV receiver to the HSI located on the PFD.
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MULTI FUNCTION DISPLAY INTERSECTION INFORMATION PAGE The Intersection Information Page displays the following information for a selected intersection: NOTE: The VOR displayed on the Intersection Information Page is the nearest VOR, not necessarily the VOR used to deﬁne the intersection.
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MULTI FUNCTION DISPLAY Intersection Information Page Operations To change the map range, turn the joystick to the left to select a lower range, turn it to the right to select a higher range. NOTE: Intersections can only be selected by identiﬁer. To select the Intersection Information Page: 1. 7-72 From any page, press and momentarily hold CLR to select the Navigation Map Page. You may skip this step if you are already viewing any of the Map Group pages. 2.
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MULTI FUNCTION DISPLAY NDB INFORMATION PAGE NDB Information Page Operations The NDB Information Page displays the following information for a selected Non-directional beacon: The NDB Information Page allows the following operations: • • • • • • Map of surrounding area NDB Identiﬁer and Symbol Name Closest city General location Latitude/longitude (degrees/minutes or degrees/ minutes/seconds), MGRS or UTM/UPS • Magnetic Variation in degrees • Frequency in kilohertz (kHz) • Nearest airport (identiﬁer, sy
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MULTI FUNCTION DISPLAY To select the NDB Information Page: 1. 2. 3. To select a NDB by using the closest city: From any page, press and hold the CLR key to select the Navigation Map Page. You may skip this step if you are already viewing any of the Map Group pages. 1. With the NDB Information Page displayed, press the FMS knob to activate the cursor. 2. Turn the large FMS knobs to highlight the closest city ﬁeld Turn the large FMS knob to select the ‘WPT’ page group.
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MULTI FUNCTION DISPLAY VOR INFORMATION PAGE VOR Information Page Operations The VOR Information Page displays the following information for a selected VOR: The VOR information page allows the following operations: • • • • • • Map of surrounding area Identiﬁer and Symbol Name Closest city General location Latitude/longitude (degrees/minutes or degrees/ minutes/seconds), MGRS or UTM/UPS • Magnetic Variation in degrees • Frequency in megahertz (MHz) • Nearest airport (identiﬁer, symbol, bearing, distance
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MULTI FUNCTION DISPLAY To select the VOR Information Page: 1. 2. 3. From any page, press and hold the CLR key to select the Navigation Map Page. You may skip this step if you are already viewing any of the Map Group pages. Turn the large FMS knob to select the ‘WPT’ page group. ‘WPT’ is displayed in the page group icon located in the lower right corner of the display. Turn the small FMS knob to select the VOR Information Page. To select a VOR by using an Identiﬁer: 1.
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MULTI FUNCTION DISPLAY USER WAYPOINT INFORMATION PAGE The G1000 allows the storage of up to 1,000 userdeﬁned waypoints. The User Waypoint Information Page displays the waypoint name (up to six characters long), identiﬁer and radial from two reference waypoints, distance from one reference waypoint, along with the user waypoints latitude/longitude position.
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MULTI FUNCTION DISPLAY To select the User Waypoint Information Page: 1. From any page, press and hold the CLR key to select the Navigation Map Page. 2. Turn the large FMS knob to select the ‘WPT’ page group. ‘WPT’ is displayed in the page group icon located in the lower right corner of the display. 3. Turn the small FMS knob to select the User Waypoint Information Page. CREATING USER WAYPOINTS User waypoints may be created from the User Waypoint Information Page or the Navigation Map Page.
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MULTI FUNCTION DISPLAY To create a new user waypoint by referencing an existing waypoint: To capture and save your present position as a user waypoint: 1. With the User Waypoint Information Page displayed, press the FMS knob to activate the cursor. 1. 2. Turn the small and large FMS knobs to enter a name for the new waypoint and press the ENT key. The message ‘Are you sure you want to create the new user waypoint’ is displayed. Press ‘YES’ to create the new waypoint.
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MULTI FUNCTION DISPLAY MODIFYING USER WAYPOINTS To modify an existing waypoint, select that waypoint on the User Waypoint Information Page and enter the new position information directly over the old information. To modify a user waypoint by changing its latitude/longitude position: 1. With the User Waypoint Information Page displayed, press the FMS knob to activate the cursor. 2. Turn the small and large FMS knobs to enter a name for the new waypoint and press the ENT key.
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MULTI FUNCTION DISPLAY USER WAYPOINT INFORMATION PAGE OPTIONS The following User Waypoint Information Page Options are available by pressing the MENU key (with the User Waypoint Information Page displayed): • • • • • • • Delete All User Waypoints View Recent User WPT List Use Present Position Auto Comment Create New user Waypoint Delete User Waypoint Rename User Waypoint ‘Delete All User Waypoints’ allows you to delete all user waypoints from memory. To delete all user waypoints: 1.
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MULTI FUNCTION DISPLAY To move the currently selected user waypoint to the present position of the aircraft: 1. Select the User Waypoint Information Page and press the MENU key to display the User Waypoint Information Page options. 2. Turn the large FMS knob to select ‘Use Present Position’ and press the ENT key. 3. Highlight the position and press the ENT key. ‘Auto Comment’ when selected will overwrite the currently selected user waypoints comment with an automatically generated comment.
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MULTI FUNCTION DISPLAY Delete User Waypoint allows the pilot to delete a user waypoint. Rename User Waypoint allows the pilot to rename a user waypoint. To delete a user waypoint: To rename a user waypoint: 1. Select the User Waypoint Information Page and press MENU to display the User Waypoint Information Page Options or press the DELETE softkey. 1. Select the User Waypoint Information Page and press MENU to display the User Waypoint Information Page Options or press the RENAME softkey. 2.
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MULTI FUNCTION DISPLAY 7.9 AUXILIARY PAGE GROUP The Auxiliary Page Group (AUX) provides detailed trip planning information, satellite status, RAIM prediction, system settings, LRU status and database information. The AUX Group page names are as follows: • • • • • Trip Planning Utility GPS Status System Setup System Status To quickly select an Aux page: 1. From any page, press and hold the CLR key to select the Navigation Map Page. 2. Turn the large FMS knob to select the ‘AUX’ page group. 3.
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MULTI FUNCTION DISPLAY TRIP PLANNING PAGE The Trip Planning Page calculates trip statistics, fuel statistics, and other statistics for a speciﬁed Direct-to, point-to-point, or ﬂight plan based on automatic or manual input of data. Figure 7-64 Trip Planning Page Menu ENT key and the ﬂashing cursor moves to the ‘to’ waypoint ﬁeld. Turn the small and large FMS knobs to enter the identiﬁer of the ‘to’ waypoint and press the ENT key to accept the waypoint. OR, 4.
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MULTI FUNCTION DISPLAY identiﬁer is entered, press the ENT key to accept the waypoint. The ﬂashing cursor moves to the to waypoint. Again, turn the small and large FMS knobs to enter the identiﬁer of the ‘to’ waypoint and press the ENT key to accept the waypoint.
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MULTI FUNCTION DISPLAY Other Statistics To calculate Density Altitude and True Airspeed 1. Select ‘MANUAL’ page mode by pressing the Manual softkey. 2. Turn the large FMS knob to select the ‘IND ALTITUDE’ ﬁeld. Turn the small and large FMS knobs to enter the altitude indicated on your altimeter. Press the ENT key when ﬁnished. 3. The ﬂashing cursor moves to the ‘PRESSURE’ ﬁeld. Turn the small and large FMS knobs to enter the barometric pressure (altimeter setting). Press the ENT key when ﬁnished. 4.
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MULTI FUNCTION DISPLAY Utility Page The Utility Page displays timers, trip statistics, and scheduler information for ﬂight planning purposes. This page intentionally left blank. Figure 7-65 Utility Page Figure 7-66 Utility Page Menu 7-88 Garmin G1000 Pilot’s Guide for the Diamond DA40 190-00592-00 Rev.
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MULTI FUNCTION DISPLAY Utility Page Operations To set the generic timer direction (up, down): 1. Select the AUX UTILITY Page. 2. Press the FMS knob. The ‘GENERIC’ timer ﬁeld is highlighted. 3. Turn the small FMS knob to display the ‘UP/ DOWN’ window. 4. Turn the small or large FMS knob to select ‘UP’ or ‘DOWN’ and press the ENT key. To start, stop, or reset the generic timer: 1. Select the AUX UTILITY Page. 2. Press the FMS knob. Turn the large FMS knob to select the ‘START?’ Field. 3.
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MULTI FUNCTION DISPLAY Trip Statistics To enter a name: To reset trip statistics readouts: 1. 2.
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MULTI FUNCTION DISPLAY GPS STATUS PAGE The GPS Status Page provides a visual reference of GPS receiver functions: Figure 7-67 GPS Status Page Figure 7-68 GPS Status Page Menu 190-00592-00 Rev.
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MULTI FUNCTION DISPLAY Satellite Status Page • Satellite constellation displaying the following for each satellite being tracked: Azimuth Elevation PRN number Tracking status • A receiver tracking status display that displays the following GPS sub-system status situations: ‘2D NAV’, when only 2-dimensional position is available ‘3D NAV’, when 3-dimensional position is available • Estimated position error • Dilution of precision • Horizontal uncertainty level • GPS calculated position • GPS calculated time
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MULTI FUNCTION DISPLAY RAIM Prediction “RAIM” is an acronym for Receiver Autonomous Integrity Monitoring, a GPS receiver function that performs a consistency check on all tracked satellites. RAIM ensures that the available satellite geometry will allow the receiver to calculate a position within a speciﬁed protection limit (2.0 nautical miles for oceanic and enroute, 1.0 NM for terminal and 0.3 NM for non-precision approaches).
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MULTI FUNCTION DISPLAY GPS Signal Strength The Satellite Status Page can be helpful in troubleshooting weak (or missing) signal levels due to poor satellite coverage or installation problems. Refer to this page occasionally to monitor GPS receiver performance and establish a normal pattern for system operation. Should problems occur at a later date, it may be helpful to have an established baseline from which to compare. To select the GPS receiver for which data is displayed: 1.
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MULTI FUNCTION DISPLAY SYSTEM SETUP PAGE The System Setup Page is the fourth AUX Page and provides access (via a list of menu options) to manage the following system parameters: • • • • • • • • • • • Local or UTC time display Units of measure settings (display units) Position Formats Map Datums Airspace Alerts Arrival Alert Audio Alerts MFD Data Bar Fields GPS CDI Range Adjustments COM Transceiver Channel Spacing. Nearest Airport Parameters Figure 7-71 System Setup Page 190-00592-00 Rev.
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MULTI FUNCTION DISPLAY Pilot Proﬁles Creating a Proﬁle The Pilot Proﬁle section of the System Setup Page allows the pilot to select, create, delete, and rename up to a total of 25 proﬁles. Proﬁles can be created based on Garmin Factory Defaults, Default Proﬁle Settings, Current System Settings, and Custom Proﬁle Settings. To create a Proﬁle: The Pilot Proﬁle section of the system setup page displays the following data: Select the System Setup Page. 2.
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MULTI FUNCTION DISPLAY Deleting a Proﬁle Date/Time To delete a proﬁle: The Date/Time box provides settings for time format (local or UTC; 12- or 24-hour) and time offset. The time offset is used to deﬁne current local time. UTC (also called “GMT” or “Zulu”) date and time are calculated directly from the GPS satellites signals and cannot be changed. If you prefer to use local time, simply designate the offset by adding or subtracting the correct number of hours. 1. Select the System Setup Page. 2.
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MULTI FUNCTION DISPLAY Display Units The Display Units section of the System Setup Page allows you to conﬁgure the displayed data to standard or metric units of measure. The Display Units section also provides two magnetic variation (heading) options: True and Auto. If ‘Auto’ is selected, all track, course and heading information is corrected to the computed magnetic variation. The “True” setting references all information to true north.
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MULTI FUNCTION DISPLAY Map Datums Airspace Alerts The Map Datum section of the System Setup Page allows selection of map datums to be used by the G1000 from a list of datums available in the current aviation database (See Appendix D for a list of available map datums). NOTE: Per TSO C129a, the WGS-84 map datum should be used in the United States. For use outside the U.S., select the geodetic datum required by that country. 1. Select the System Setup Page. 2.
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MULTI FUNCTION DISPLAY To turn an Airspace Alert on or off: Arrival Alerts 1. Select the System Setup Page. 2. Press the FMS knob momentarily, to activate the ﬂashing cursor. 3. Turn the large FMS knob to highlight the desired ‘AIRSPACE ALERTS’ ﬁeld. 4. Turn the small FMS knob to display the options list.
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MULTI FUNCTION DISPLAY Audio Alerts MFD Data Bar Fields The Audio Alert section of the System Setup Page gives you the option of selecting a male or female voice for audio alerts. The MFD Nav Data Bar Fields section of the System Setup Page displays the current conﬁguration of the Nav data (MFD) bar ﬁelds. The Nav Data Bar Fields section of the System Setup Page allows you to conﬁgure the four Nav data bar ﬁelds to the following values: To change the audio alert voice: 1. Select the System Setup Page.
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MULTI FUNCTION DISPLAY GPS CDI To change the CDI range: The CDI section of the System Setup Page allows you to deﬁne the range for the on-screen course deviation indicator. The range values represent full range deﬂection for the CDI to either side. The default setting is ‘AUTO’. At this setting, the CDI range is set to 5.0 nautical miles during the “enroute” phase of ﬂight. Within 30 nm of your destination airport, the CDI range gradually ramps down to 1.0 nm (terminal area).
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MULTI FUNCTION DISPLAY COM Conﬁguration COM Conﬁguration allows you to select 8.33 kHz or 25.0 kHz COM frequency channel spacing. NOTE: 8.33 kHz VHF communication frequency channel spacing is not approved for use in the United States. Select the 25.0 kHz channel spacing option for use in the United States. To change COM channel spacing: To select Nearest airport surface matching criteria (any, hard only, hard/soft, water): 1. Select the System Setup Page. 2.
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MULTI FUNCTION DISPLAY SYSTEM STATUS PAGE The System Status Page displays the status and software version numbers for all detected system LRUs. Pertinent information of all databases in the system is also displayed. Active LRUs are indicated by a green check mark and failed LRUs are indicated by a red X. The Pilot should note the failed LRU and inform a Diamond service center or Garmin dealer. Figure 7-72 System Status Page 7-104 Garmin G1000 Pilot’s Guide for the Diamond DA40 190-00592-00 Rev.
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MULTI FUNCTION DISPLAY 7.10 NEAREST PAGE GROUP The nearest (NRST) page group is the fourth page group which consists of the following pages: • • • • • • • Nearest Airports Nearest Intersections Nearest NDB Nearest VOR Nearest User WPTS Nearest Frequencies Nearest Airspaces The NRST pages can be used in conjunction with the Direct-to function to quickly set a course to a nearby facility. This feature can be a real time saver compared to retrieving information from the database using the WPT pages.
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MULTI FUNCTION DISPLAY To select a nearby airport, VOR, NDB, intersection or user waypoint as a Direct-to destination: 1. Use the ﬂashing cursor to scroll through a NRST page list and highlight the desired nearest waypoint. 2. Press the Direct-to key to display the Direct-to Page. 3. Press the ENT key to accept the selected waypoints identiﬁer and press the ENT key a second time (with ‘Activate?’ highlighted) to begin navigating to the selected waypoint.
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MULTI FUNCTION DISPLAY NEAREST AIRPORTS PAGE To select the Nearest Airports Page: The Nearest Airports Page displays the following information for a selected airport: • Map of surrounding area • Airport Identiﬁer, Symbol, Bearing, Distance (up to 25 airports within 200 nm of current position) • Name • Closest city • Elevation • Runway information • Airport COM frequencies • Approaches 1. From any page, press and hold the CLR key to select the Navigation Map Page. 2.
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MULTI FUNCTION DISPLAY To select a nearest airport from the Nearest Airports Page: 1. 2. Press the APT softkey located at the bottom of the display. The ﬁrst airport in the nearest airports list is highlighted. Turn the large FMS knob to highlight the desired airport. The remaining information on the Nearest Airports Page pertains to the selected airport. To select a runway from the Nearest Airports Page: 1. Press the RNWY softkey located at the bottom of the display. 2.
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MULTI FUNCTION DISPLAY NEAREST INTERSECTIONS PAGE The Nearest Intersections Page displays the following information for a selected intersection: • Map of surrounding area • Intersection identiﬁer, Symbol, Bearing, Distance (within 200 nm of current position) • Lat/Lon (latitiude/longitude) • Reference VOR Information consisting of: • VOR Name • Symbol • Frequency • Bearing • Distance To select the Nearest Intersections Page: 1. From any page, press and hold the CLR key to select the Navigation Map Page.
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MULTI FUNCTION DISPLAY NEAREST NDB PAGE To select the Nearest NDB Page: The Nearest NDB Page displays the following information for a selected NDB: • Map of surrounding area • NDB Identiﬁer, Symbol, Bearing, Distance (within 200 nm of current position) • NDB Name • Latitude/longitude (degrees/minutes or degrees/ minutes/seconds) • Frequency 1. From any page, press and hold the CLR key to select the Navigation Map Page. 2. Turn the large FMS knob to select the NRST page group.
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MULTI FUNCTION DISPLAY NEAREST VOR PAGE To select the Nearest VOR Page: The VOR Information Page displays the following information for a selected VOR: • • • • • • Map of surrounding area Identiﬁer, Symbol, Bearing, Distance Name Closest city VOR Type Latitude/longitude (degrees/minutes or degrees/ minutes/seconds) • Magnetic Variation in degrees • Frequency in megahertz (MHz) 1. From any page, press and hold the CLR key to select the Navigation Map Page. 2.
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MULTI FUNCTION DISPLAY To select a nearest VOR from the Nearest VOR Page: 1. Select the Nearest VOR Page. 2. Press the VOR softkey and turn either the small or large FMS knob, or press the ENT key to select a VOR. OR Press the MENU key. Select the Select VOR Window option and press the ENT key. Turn either the small or large FMS knob to select a VOR. 7-112 The remaining information on the Nearest VOR Page pertains to the selected VOR. To select and load a VOR frequency from the Nearest VOR Page: 1.
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MULTI FUNCTION DISPLAY NEAREST USER WAYPOINT PAGE The Nearest User Waypoint Page displays the following information for a selected User Waypoint: • • • • • • Map of surrounding area Identiﬁer Symbol Bearing and Distance Latitude/longitude A reference waypoint with identiﬁer, bearing, and distance • Waypoint Comment • A second reference waypoint with identiﬁer and bearing To select the Nearest User Waypoint Page: 1. From any page, press and hold the CLR key to select the Navigation Map Page. 2.
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MULTI FUNCTION DISPLAY NEAREST FREQUENCIES PAGE The Nearest Frequencies Page displays the facility name, bearing to and distance to the ﬁve nearest ARTCC and FSS points of communication (within 200 nautical miles of the present position). For each ARTCC and FSS listed, the Nearest Frequencies Page also indicates the frequency and may be used to quickly tune the COM transceiver to the facility frequency.
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MULTI FUNCTION DISPLAY NEAREST AIRSPACES PAGE To select the Nearest Airspaces Page: The Nearest Airspaces Page displays the following information for a maximum of 20 controlled or special use airspaces: • Map of surrounding area • Airspace Alerts Box displaying Airspace Name, Status, and Time to Entry • Airspace and Agency • Vertical Limits (ﬂoor/ceiling) • Airspace Frequencies 1. From any page, press and hold the CLR key to select the Navigation Map Page. 2.
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MULTI FUNCTION DISPLAY Airspace Alerts Box The Airspace Alerts Box displays the Airspace Name, Status, and Time to Entry. The status and time to entry (if applicable) is based on the following conditions: • If the projected course will take the aircraft inside an airspace within the next ten minutes, the status ﬁeld shows the airspace as ‘Ahead’.
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MULTI FUNCTION DISPLAY Airspaces The following airspace types are displayed on the Nearest Airspaces Page along with messages in the Airspace Alerts Box: • • • • • • • • • • • • • • Alert Caution Class B Class C TCA Danger MOA Prohibited Restricted TMA Training TRSA Unspeciﬁed Warning 190-00592-00 Rev. A The Nearest Airspaces Page also displays the ﬂoor and ceiling limits of the airspace. The following are examples of what may appear as vertical limits for an airspace: • • • • • • • • 5,000 ft.
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G1000 TM Optional Equipment
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Garmin G1000 Pilot’s Guide for the Diamond DA40 190-00592-00 Rev.
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OPTIONAL EQUIPMENT 8.1 INTRODUCTION NOTE: Not all optional equipment is available on each airframe. Refer to the approved Aircraft Flight Manual Supplement (AFMS) for more information.
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OPTIONAL EQUIPMENT 8.2 STORMSCOPE NOTE: Refer to the WX-500 User’s Guide for a detailed description of Stormscope operation. The Navigation Map Page (Figure 8-1) displays cell or strike data using the yellow lightning strike symbology shown in Table 8-1. DISPLAYING STORMSCOPE LIGHTNING DATA ON THE NAVIGATION MAP PAGE NOTE: Stormscope must receive valid heading information for Stormscope lightning data to be displayed on the G1000.
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OPTIONAL EQUIPMENT To display Stormscope Lightning Data on the Navigation Map Page: 1. Press the MAP softkey. 2. Press the STRMSCP softkey (pressing the STRMSCP softkey again removes Stormscope Lightning Data from the Navigation Map Page). NOTE: At a map range of less than 25 nm, Stormscope lightning data is not displayed but can still be present. The presence of Stormscope lightning data is indicated by the annunciation in the upper right hand corner ‘LTNG < 25 nm’ (Figure 8-2).
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OPTIONAL EQUIPMENT To display the Weather Group Options: 1. 2. With the Navigation Map Page displayed, press the MENU key to display the Navigation Map Setup Menu. The cursor ﬂashes on the ‘Map Setup’ option. Press the ENT key. The Map Setup Menu is displayed. Turn the small FMS knob to select the ‘Weather’ group. To select a Stormscope lightning symbol zoom range: 1. With the Weather Group selected, press the ENT key. The cursor flashes on ‘STRMSCP LTNG. 2.
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OPTIONAL EQUIPMENT NOTE: Periodically clearing Stormscope lightning data while monitoring thunderstorms is a good way to determine if a storm is building or dissipating. Stormscope lightning data in a building storm will reappear faster and in larger numbers. Stormscope lightning data in a dissipating storm will appear slower and in smaller numbers. STORMSCOPE PAGE Stormscope lightning data is displayed on the Stormscope Page in addition to the Navigation Map Page. To select the Stormscope Page: 1.
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OPTIONAL EQUIPMENT To change the Stormscope lightning mode between ‘cell’ and ‘strike’: To change the viewing mode between 360˚ and 120˚: 1. Select the Stormscope Page. 1. Select the Stormscope Page. 2. Press the MODE softkey. The CELL and STRIKE softkeys are displayed. Press the CELL softkey to display ‘CELL’ data or press the STRIKE softkey to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box located in the upper left corner of the Stormscope Page 2. Press the VIEW softkey.
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OPTIONAL EQUIPMENT 8.3 TRAFFIC ADVISORY SYSTEMS NOTE: This addendum assumes the user has experience operating the G1000 Multi Function Display and is familiar with the applicable Trafﬁc System Pilot’s Guide. NOTE: This section describes the G1000 for TAS only. The Multi Function Display section describes the standard TIS interface. To conﬁgure TAS trafﬁc on the Navigation Map Page: 1. Select the Navigation Map Page. 2. Press MENU to display the Page Menu.
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OPTIONAL EQUIPMENT Trafﬁc Map Page (Figure 8-7) Monitoring Trafﬁc The Trafﬁc Map Page controls the source of trafﬁc data on the Navigation Map Page. NOTE: When the G1000 is conﬁgured for TAS, the system only receives TAS trafﬁc. Otherwise, if TAS is not conﬁgured, the system provides TIS trafﬁc data. To select the Trafﬁc Map Page: 1. 2. Turn the large FMS knob until the Map Page group is selected. Turn the small FMS knob until the Trafﬁc Map page is selected.
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OPTIONAL EQUIPMENT L-3 SKYWATCH TRAFFIC ADVISORY SYSTEMS (SKY497 AND SKY899) NOTE: Refer to the SKYWATCH User’s Guide for a detailed description of Skywatch operation. Power-up Self-Test Check for the following test criteria on the Trafﬁc Map Page during power-up: 1. 2. 3. The unit must be in operating mode for trafﬁc to be displayed. The ability to switch out of standby into operating mode on the ground is especially useful for scanning the airspace around the airport before takeoff.
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OPTIONAL EQUIPMENT Trafﬁc Map Page Display Range • A Trafﬁc Advisory (yellow circle) appears at 9 o’clock, range of 2 miles, 200 feet below and climbing. The pilot can change the display range on the Trafﬁc Map Page at any time. • Proximity Traffic (solid white diamond) appears at 1 o’clock, range 3.6 miles, 1000 feet below, descending. To change the display range on the Trafﬁc Page: Turn the RNG knob to zoom through the following range options: • SKYWATCH (SKY 497)—2 nm, 2 and 6 nm, 6 and 12 nm.
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OPTIONAL EQUIPMENT To switch into Standby Mode from the Trafﬁc Page: Press the STANDBY softkey. Altitude Display Mode To change the Altitude Display Mode: Press the ALT MODE softkey then press one of the following options: BELOW, NORMAL, ABOVE, UNREST. With each selection, the screen changes to display the trafﬁc detected within the selected altitude display range. The G1000 screen also displays unrestricted trafﬁc (UNREST) having a range of maximum speciﬁed by the KTA 870/KMH 880 Pilot’s Guide.
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OPTIONAL EQUIPMENT 8.4 GDL 69/69A INTRODUCTION The Garmin GDL 69/69A receiver interfaces with the G1000 to bring XM Weather and XM Digital Audio Entertainment to the cockpit. XM Weather and XM Radio operate in the S-band frequency range to provide continuous uplink capabilities at any altitude throughout North America. IMPORTANT: Before the GDL 69/69A can be used, it has to be activated by XM Satellite Radio.
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OPTIONAL EQUIPMENT Navigation Map Page Weather Control Softkeys To display weather data on the Navigation Map Page: The following softkeys control the display of NEXRAD and XM Lightning weather products on the Navigation Map Page: 1. Press the MAP softkey. 2. Press the NEXRAD or XM LTNG softkey to display the desired weather. Press the applicable softkey again to remove weather data from the Navigation Map Page. NEXRAD – Press to display NEXRAD weather and coverage information.
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OPTIONAL EQUIPMENT Navigation Map Setup Options (Figure 8-10) To customize the Navigation Map Page: The user can customize the display of XM weather on the Navigation Map Page by using the Map Setup Weather Group Options Menu. The following options are available: 1. Press the Menu key on the Navigation Map Page. 2. Select ‘Map Setup’ and press the ENT key. 3. Turn the small FMS knob to display the group selection window. Turn the small FMS knob to select the ‘Weather Group’ and press the ENT key.
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OPTIONAL EQUIPMENT NOTE: TAF is an airport forecast. TAF is generally standard around the world. TAF forecasts signiﬁcant weather changes, temporary changes, probable changes and expected changes in weather conditions.. To display METAR and TAF text on the Airport Information Page: 1. Turn the large FMS knob to select the WPT Page Group. 2. Turn the small FMS knob to select the Airport Information Page. 3.
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OPTIONAL EQUIPMENT To select the Weather Data Link Page: 1. Turn the large FMS knob to select the Map Page Group. 2. Turn the small FMS knob to select the Weather Data Link Page. Weather Data Link Page Softkeys The following softkeys perform the GDL 69/69A weather functions on the Weather Data Link Page: NEXRAD – Press to show NEXRAD weather and radar coverage information (both are activated at the same time). Composite data from all of the NEXRAD radar sites in the United States is shown.
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OPTIONAL EQUIPMENT ECHO TOP – Press to show the location, elevation, and direction of the highest radar echo. This may not indicate the top of a storm or clouds, only the highest radar return echo. The information is derived from NEXRAD information and indicates the highest altitude at which precipitation is falling. ECHO TOPS and Radar coverage are activated at the same time.
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OPTIONAL EQUIPMENT SIG/AIR – Press to show SIGMET and AIRMET information to advise the pilot of potentially hazardous weather. The advisory covers an area of at least 3,000 square miles at any one time. The update rate is every 12 minutes. NOTE: SIGMETs are broadcast for hazardous weather that is considered of extreme importance to all aircraft.
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OPTIONAL EQUIPMENT LEGEND – Press to display the Weather Legend Window. Turn the small or large FMS knob to scroll up or down through the legend list. Press the small or large FMS knob or the ENT key to remove the legend display. The Weather Legends Window describes the graphic symbols and color coding of the information for each product that is active. SFC – Press for Surface Analysis to show current or forecast conditions. The city forecasts information is combined with the surface conditions.
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OPTIONAL EQUIPMENT NOTE: When no data is shown at a given altitude for any of the weather features, the data for that altitude has not been received or the data is out of date and has been removed from the display. Wait for the next update. The update rate is every 12 minutes. WIND – Press to show wind speed and direction at a selected altitude from the ground up to 42,000 feet in 3,000 foot increments. The WIND softkey label changes to reﬂect the winds aloft altitude selected.
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OPTIONAL EQUIPMENT To display information for selected weather products: 1. Push in the joystick to display the panning arrow. 2. Move the joystick to place the panning arrow on the desired product. Press the ENT key to display pertinent information for the selected product. Note that pressing the ENT key when panning over an AIRMET or a SIGMET displays an information box that gives the actual text of that alert.
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OPTIONAL EQUIPMENT Weather Product Age (Table 8-2) The times for each of the enabled products are displayed on the right side of the display. Times are based on Zulu times when the data was assembled on the ground, not the time the data was received by the FIS sensor. When the age of a weather product is greater than half of the expiration time, the product time will change from cyan to amber in color. Current weather products use an age stamp, ‘Age: _ _ _’ in minutes.
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OPTIONAL EQUIPMENT GDL 69/69A – XM DIGITAL AUDIO ENTERTAINMENT XM Information Page Digital audio entertainment is available through the XM Satellite Radio Service using the GDL 69/69A. XM Satellite Radio allows for a variety of radio programming over long distances without having to constantly search for new stations. Based on signals from satellites, coverage far exceeds land-based transmissions. The XM Information Page provides XM Radio identiﬁcation numbers, service level, and weather products.
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OPTIONAL EQUIPMENT Data and Audio Radio ID XM RADIO PAGE Each GDL 69/69A contains a unique Data Radio ID and Audio Radio ID that allows XM to communicate with the radio. The owner must activate XM service by providing the Radio ID(s) to XM to authorize the installed services for that radio. The XM Radio Page (Figure 8-14) provides information and control of the audio entertainment features of the XM Satellite Radio.
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OPTIONAL EQUIPMENT Active Channel Category The Active Channel ﬁeld on the XM Radio Page displays the currently selected channel that the XM Radio is using. The Channel feature is used to navigate through the channels in the selected category. You can step through the channels one at a time or you may also select a channel directly by channel number. The ‘Category’ ﬁeld of the XM Radio Page displays the currently selected category of audio.
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OPTIONAL EQUIPMENT Volume Presets The Volume ‘control’ (Figure 8-16) sets the audio volume level, as well as mutes the audio. Pressing the VOL softkey brings up the Volume bar graph, muting softkey, and the Volume control softkeys. Up to 15 channels from any category can be assigned a preset number. The preset channel can then be selected directly and added to the Active Channel list for listening. To set a preset channel number: 1.
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OPTIONAL EQUIPMENT GDL 69/69A TROUBLESHOOTING Although it is the responsibility of the facility that installed the GDL 69/69A to correct any hardware problems, the user can perform some quick troubleshooting steps to ﬁnd the possible cause of a failure. First, ensure that the owner/operator of the aircraft in which the GDL 69/69A is installed has subscribed to XM Radio, and that it has been activated. Perform a quick check of the circuit breakers to ensure the GDL 69/69A has power applied.
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G1000 TM Annunciations and Alerts
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Garmin G1000 Pilot’s Guide for the Diamond DA40 190-00592-00 Rev.
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ANNUNCIATIONS & ALERTS 9.1 INTRODUCTION NOTE: The Aircraft Flight Manual Supplement (AFMS) takes precedence over any conﬂicting information found in this document. The G1000 Alerting System conveys alerts to the pilot using the following: • Annunciation Window: The Annunciation window displays abbreviated annunciation text. Text is colored based on alert levels described in the Alert Level Deﬁnitions section.
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ANNUNCIATIONS & ALERTS 9.2 ALERT LEVEL DEFINITIONS The G1000 Alerting System, as installed in the Diamond DA40, DA40F and DA40D models, uses four alert levels: • WARNING: This level of alert requires immediate pilot attention. A warning alert is accompanied by an annunciation in the Annunciation window along with a continuous aural tone. Warning alert text is RED. A warning alert is also accompanied by a ﬂashing WARNING softkey annunciation.
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ANNUNCIATIONS & ALERTS 9.3 DA40 & DA40F AIRCRAFT ALERTS The following alerts are conﬁgured speciﬁcally for the Diamond DA40 & DA40F. See the Aircraft Flight Manual Supplement (AFMS) for recommended pilot actions. WARNING Alerts Annunciation Window Text Alerts Window Message OIL PRES LO Oil pressure is below 25 psi. FUEL PRES LO * Fuel pressure is below 14 psi. FUEL PRES HI * Fuel pressure is greater than 35 psi. ALTERNATOR Alternator failed. Battery is only electrical source.
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ANNUNCIATIONS & ALERTS Message Advisory Alerts Alerts Window Message PFD FAN FAIL – The cooling fan for the PFD is inoperative. MFD FAN FAIL – The cooling fan for the MFD is inoperative. GIA FAN FAIL – The cooling fan for the GIAs is inoperative. Audio Alert None None None Voice Alerts The following voice alerts can be conﬁgured for ‘Male’ or ‘Female’ gender by using the AUX System Setup Page on the MFD.
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ANNUNCIATIONS & ALERTS 9.4 DA40D AIRCRAFT ALERTS The following alerts are conﬁgured speciﬁcally for the Diamond DA40D. See the Aircraft Flight Manual Supplement (AFMS) for recommended pilot actions. WARNING Alerts Annunciation Window Text ENG TEMP OIL TEMP OIL PRES GBOX TEMP ALTN AMPS ALTN FAIL STARTER L / R FUEL TEMP DOOR OPEN AP TRIM FAIL Alerts Window Message Engine coolant temp is >105 deg C. Engine oil temp is greater than 140 deg C. Engine oil pressure is less than 1.2 bar.
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ANNUNCIATIONS & ALERTS Annunciation Advisory Alerts Annunciation Window Text GLOW ON FUEL XFER Alerts Window Message Engine glow plug active. Fuel transfer in progress. Audio Alert No Tone No Tone Message Advisory Alerts Alerts Window Message PFD FAN FAIL – The cooling fan for the PFD is inoperative. MFD FAN FAIL – The cooling fan for the MFD is inoperative. GIA FAN FAIL – The cooling fan for the GIAs is inoperative.
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ANNUNCIATIONS & ALERTS 9.5 G1000 SYSTEM ANNUNCIATIONS When an LRU or an LRU function fails, a large red ‘X’ is typically displayed on windows associated with the failed data. The following section describes various system annunciations. Refer to the Aircraft Flight Manual Supplement (AFMS) for additional information regarding pilot responses to these annunciations. System Annunciation NOTE: Upon power-up of the G1000 system, certain windows remain invalid as G1000 equipment begins to initialize.
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ANNUNCIATIONS & ALERTS System Annunciation Comment Display system is not receiving vertical speed input from the air data computer. Display system is not receiving valid heading input from the AHRS. Display system is not receiving valid OAT information from the air data computer. Display system is not receiving valid true airspeed information from the air data computer. GPS information is either not present or is invalid for navigation use.
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ANNUNCIATIONS & ALERTS A red ‘X’ may be the result of an LRU or an LRU function failure. The ﬁgure presented below illustrates all possible ﬂags and the responsible LRUs.
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ANNUNCIATIONS & ALERTS 9.6 G1000 SYSTEM MESSAGE ADVISORIES This section describes various G1000 system message advisories. Certain messages are issued due to an LRU or LRU function failure. Such messages are normally accompanied by a corresponding red ‘X’ annunciation as shown previously in the G1000 System Annunciations section. NOTE: This section provides information regarding G1000 message advisories that may be displayed by the system.
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ANNUNCIATIONS & ALERTS MFD & PFD Message Advisories (Cont.) Message Comments PFD1 “KEY” KEYSTK – key is stuck. A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by pressing MFD1 “KEY” KEYSTK – key is stuck. it several times. If the problem persists, the G1000 system should be serviced. CNFG MODULE – PFD1 conﬁguration The PFD1 conﬁguration module backup memory has failed. Have the G1000 system module is inoperative. serviced.
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ANNUNCIATIONS & ALERTS GMA 1347 Message Advisories Alerts Window Message GMA1 FAIL – GMA1 is inoperative. Comments The audio panel self-test has detected a failure. The audio panel is unavailable. The G1000 system should be serviced. GMA1 CONFIG – GMA1 conﬁguration The audio panel conﬁguration settings do not match backup conﬁguration memory. error. Conﬁg service req’d. The G1000 system should be serviced. MANIFEST – GMA1 software The audio panel has incorrect software installed.
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ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments MANIFEST – GIA1 software mismatch. Communication halted. The GIA1 and/or GIA 2 has incorrect software installed. The G1000 system should MANIFEST – GIA2 software mismatch. be serviced. Communication halted. COM1 TEMP – COM1 over temp. The system has detected an over-temperature condition in COM1 and/or COM2. The Reducing transmitter power. transmitter is operating at reduced power.
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ANNUNCIATIONS & ALERTS GIA 63 Message Advisories (Cont.) Alerts Window Message Comments GPS1 SERVICE – GPS1 needs service. Return unit for repair. A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still GPS2 SERVICE – GPS2 needs service. be available. The G1000 system should be serviced. Return unit for repair. NAV1 SERVICE – NAV1 needs service. Return unit for repair. A failure has been detected in the NAV1 and/or NAV2 receiver.
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ANNUNCIATIONS & ALERTS GTX 33 Message Advisories Alerts Window Message XPDR1 CONFIG – XPDR1 conﬁg error. Conﬁg service req’d. MANIFEST – GTX1 software mismatch. Communication halted. BACKUP PATH – Transponder using backup data path. Comments The transponder conﬁguration settings do not match those of the backup conﬁguration memory. The G1000 system should be serviced. The transponder has incorrect software installed. The G1000 system should be serviced.
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ANNUNCIATIONS & ALERTS GMU 44 Message Advisories Alerts Window Message HDG FAULT – A magnetometer fault has occurred. MANIFEST – GMU1 software mismatch. Communication halted. Comments A fault has occurred in the GMU 44. Heading is ﬂagged as invalid. The AHRS uses GPS for backup mode operation. The G1000 system should be serviced. The GMU 44 has incorrect software installed. The G1000 system should be serviced.
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ANNUNCIATIONS & ALERTS Miscellaneous Message Advisories (Cont.) Alerts Window Message Comments APPR VPROF – Approaching VNAV Aircraft is approaching VNAV proﬁle. Prepare to climb or descend to meet VNAV proﬁle. proﬁle. APPR TRG ALT – Approaching target Aircraft is approaching target altitude. Prepare to level aircraft. altitude. LOCKED FPL – Cannot navigate locked This occurs when the pilot attempts to activate a stored ﬂight plan that contains ﬂight plan. locked waypoints.
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G1000 TM Appendices
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APPENDIX A SD CARD USE 4. The G1000 system uses Secure Digital (SD) cards to load and store various types of data. For basic ﬂight operations, SD cards are required for terrain database storage as well as aviation database updates. After the update completes, the PFD starts in normal mode. Remove the aviation database update SD card from the PFD. 5. Turn the G1000 system OFF. 6. Repeat steps 1 through 4 for the MFD. The MFD and PFD aviation databases are now updated. 7.
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APPENDIX A The obstacle and terrain database updates can be obtained by following the instructions detailing in the ‘Aviation Databases’ section of the Garmin website (www.garmin.com). Once the updated ﬁles have been downloaded from the website, a PC equipped with an appropriate SD card reader is used to unpack and program the new databases onto the existing Supplemental Data Cards. Equipment required to perform the update is as follows: • Windows-compatible PC computer (Windows 2000 or XP recommended).
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APPENDIX B Abbreviation or Acronym ADF AF AFM AFMS AGL AHRS AIM AIRMET ALT AMPS ANNUNC APPR APR APT ARINC ARSPC ARTCC ARV AS ASB ATC ATCRBS AUTOSEQ AUX Deﬁnition Automatic Direction Finder Arc to ﬁx Aircraft Flight Manual Aircraft Flight Manual Supplement Above Ground Level Attitude and Heading Reference System Airman’s Information Manual Airman’s Meteorological Information Altitude Amperes Annunciation Approach Approach Airport Aeronautical Radio Incorporated Airspace Air Route Trafﬁc Control Center Arriv
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APPENDIX B B-2 Abbreviation or Acronym FMS FOB FPL FPM FREQ FRZ FSS ft Deﬁnition Flight Management System Fuel On Board Flight Plan Feet Per Minute Frequency Freezing Flight Service Station Foot/feet G/S GAL GDC GDU GEA GIA GL GMU GND GPH GPS GRS GS GTX Glideslope Gallon(s) Garmin Air Data Computer Garmin Display Unit Garmin Engine/Airframe Unit Garmin Integrated Avionics Unit Gallon(s) Garmin Magnetometer Unit Ground Gallons per Hour Global Positioning System Garmin Reference System Ground Speed Garmi
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APPENDIX B Abbreviation or Acronym NDB Nexrad nm NRST Deﬁnition Non-directional Beacon Next Generation Radar Nautical Mile(s) Nearest O OAT OBS Outer Marker Outside Air Temperature Omni Bearing Selector P ALT PA PASS PFD PI POSN P.
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APPENDIX B B-4 Abbreviation or Acronym VD VERT VFR VHF VI VLOC VM VMC VNAV VOL VOR VPROF VR VS Vspeed Deﬁnition Heading Vector to DME Distance Vertical Visual Flight Rules Very High Frequency Heading Vector to Intercept VOR/Localizer Receiver Heading Vector to Manual Termination Visual Meteorological Conditions Vertical Navigation Volume VHF Omnidirectional Range VNAV Proﬁle Heading Vector to Radial Vertical Speed Airspeed WAAS WGS-84 WPT WPTS WW WX Wide Area Augmentation System World Geodetic System -
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APPENDIX B Navigation Term Bearing Calibrated Airpseed Course Course to Steer Crosstrack Error Cumulative Distance Dillution of Precision Desired Track Efﬁciency Endurance Enroute Safe Altitude Estimated Position Error Estimated Time of Arrival Estimated Time Enroute Fuel Flow Fuel On Board Groundspeed Heading 190-00592-00 Rev. A Deﬁnition The compass direction from your present position to a destination waypoint. Indicated airspeed corrected for installation and instrument errors.
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APPENDIX C QUESTIONS & ANSWERS This Appendix answers common questions regarding G1000 system operational capabilities. If a particular subject is not covered in this Appendix, the index may be used to ﬁnd the appropriate section in this manual. If a sufﬁcient answer is still not found, an authorized Garmin dealer or contact Garmin directly (see Copyright page). Garmin is dedicated to supporting its products and customers.
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APPENDIX C mation from the current database to deﬁne the waypoints. If the database is changed or updated, the G1000 system automatically updates the information, provided the procedure has not been modiﬁed. Should an approach, departure, or arrival procedure no longer be available, the ﬂight plan becomes locked until the procedure is deleted from the ﬂight plan. Can “slant Golf” (“/G”) be filed using the G1000? “/G” may be ﬁled for a ﬂight plan.
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APPENDIX C Why does the G1000 not automatically sequence to the next waypoint? The G1000 only sequences ﬂight plan waypoints when automatic sequencing is enabled (i.e., no “OBS” or “SUSP” annunciation). For automatic sequencing to occur, the aircraft must also cross the “bisector” of the turn being navigated. The bisector is a perpendicular line between two ﬂight plan legs which crosses through the waypoint common to both legs.
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APPENDIX C After a missed approach, how can the same approach be re-selected? How can a new approach be activated? After ﬂying the missed approach procedure, the pilot may reactivate the same approach for another attempt from the Procedures Page. Once the clearance is given for another attempt, activate the approach from the Procedures Page by highlighting “Activate Approach?”, then pressing the ENT key.
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APPENDIX D G1000 MAP DATUMS The G1000 system supports the following map datums. WARNING: WGS 84 is the default datum and should be used in all situations except when another datum is speciﬁcally required for safe navigation. Pilots using map datums other than WGS 84 do so at their own risk.
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APPENDIX D G1000 MAP DATUMS (CONT.
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APPENDIX E GENERAL TIS INFORMATION INTRODUCTION The Trafﬁc Information Service (TIS) provides trafﬁc advisory information in the cockpit of non-TCAS equipped aircraft. TIS is a ground-based service providing relative location of all ATCRBS Mode-A and Mode-C transponder equipped aircraft within a speciﬁed service volume. The TIS ground sensor uses real time track reports to generate trafﬁc notiﬁcation. The G1000 system displays TIS trafﬁc information on the Trafﬁc Map Page of the MFD.
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APPENDIX E NOTE: TIS is unavailable at low altitudes in many areas of the United States. This is often the case in mountainous regions. TIS information is collected during a single radar sweep. Collected information is then sent through the Mode S uplink on the next radar sweep. Because of this, the surveillance information is approximately ﬁve seconds old. TIS ground station tracking software uses prediction algorithms to compensate for this delay.
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APPENDIX F MAP SYMBOLS BASEMAP AIRPORT Item Interstate Highway – 2-digit drawn inside Item Symbol Symbol Unknown Airport Interstate Highway – 3-digit drawn inside Non-towered, Non-serviced Airport State Highway – 2-digit drawn inside Towered, Non-serviced Airport State Highway – 3-digit drawn inside Non-towered, Serviced Airport State Highway – 4-digit drawn inside State Highway – 5-digit drawn inside Towered, Serviced Airport US Highway – 2-digit drawn inside Restricted (Private) Airport U
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APPENDIX F TRAFFIC MISCELLANEOUS Item Symbol Trafﬁc Item ARTCC Frequency or FSS Frequency Proximate Trafﬁc Default Map Cursor Symbol Elevation Pointer Cursor Trafﬁc Advisory, Out of Range Measuring Cursor Trafﬁc Advisory Overzoom Indicator (map toolbar) LIGHTNING STRIKE Terrain Proximity Enabled (map toolbar) Item Lightning Strike – Age is 0-6 Seconds Symbol Trafﬁc Enabled (map toolbar) User Waypoint Wind Vector Lightning Strike – Age is 6-20 Seconds Lightning Strike – Age is 20-60 Seconds
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APPENDIX F LINE SYMBOLS Item ICAO Control Area Class B Airspace Symbol Mode C Tower Area Warning Area Alert Area Caution Area Danger Area Prohibited Area Restricted Area Training Area Unknown Area Class C Terminal Radar Service Area Mode C Area Military Operations Area (MOA) State or Province Border International Border Road Railroad Lattitude/Longitude 190-00592-00 Rev.
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APPENDIX F OBSTACLE DATABASE Obstacle Color RED YELLOW GRAY Indication WARNING: Obstacle height is at or above 100 ft below the current aircraft altitude. CAUTION: Obstacle height is between 100 ft and 1000 ft below the current aircraft altitude. SAFE: Obstacle height is lower than 1000 ft below the current aircraft altitude.
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APPENDIX G G1000 SYSTEM SPECIFICATIONS GDU 1040 MFD & PFD GIA 63 INTEGRATED AVIONICS UNITS Physical Speciﬁcations Physical Speciﬁcations Height: Width: Depth: Weight: Voltage Range: Display: 7.70 inches (19.56 cm) 11.80 inches (29.97 cm) 3.55 inches (9.02 cm) 6.6 lb (2.99 kg) 9 – 33 Vdc 10.
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APPENDIX G GDC 74A AIR DATA COMPUTER Physical Speciﬁcations Physical Speciﬁcations Height: Width: Length: Weight: Voltage Range: 3.23 inches (8.20 cm) 3.05 inches (7.75 cm) 6.45 inches (16.38 cm) 1.69 lb (0.77 kg) 10 – 33 Vdc Pressure Altitude Range: -1,400 feet to 50,000 feet Vertical Speed Range: -20,000 fpm to +20,000 fpm Airspeed Range: 450 knots Airspeed Mach Range: <1.00 Mach Total Air Temperature Range: -85º C to +85º C GTX 33 MODE S TRANSPONDER Physical Speciﬁcations 6.30 inches (16.0 cm) 1.
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APPENDIX G GRS 77 AHRS AHRS Performance Physical Speciﬁcations Height: Width: Length: Weight: Voltage Range: 3.25 inches (8.36 cm) 3.75 inches (9.53 cm) 8.5 inches (21.59 cm) 2.40 lb (1.08 kg) 10 – 33 Vdc Bank/Pitch Error: Maneuvers Range: Rotation Rate: Heading: ±1.
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G1000 TM Index
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INDEX A Active Flight Plan Page 7-39–7-40 Active frequency 3-2 ADF 2-19–2-20, 3-1, 3-9–3-11 ADF/DME Tuning window 3-9 Advisory 2-44–2-45, 9-2 ADVISORY softkey 2-45 Aircraft Alerts DA40/DA40F 9-3 DA40D 9-5 Airman’s Meteorological information (AIRMET) 8-18, 8-21, 8-27 Airport frequency 7-108 Airport Frequency Information ﬁeld 7-63 Airport information 3-15 Airport information window 2-31 Airport Runway Information ﬁeld 7-64 Airport Symbols 7-9 Airspace 7-9 Airspace boundaries 7-23 Airspace messages 7-117 Airsp
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INDEX Cyclones 8-27 CYCLONE softkey 8-20 Cylinder Head Temperature (CHT) 6-2, 6-4 CYL SLCT softkey 6-4 D Database 1-10, A-1 Date/Time box 7-97 DCLTR softkey 2-5–2-7 Declutter 2-5, 2-25, 7-10 DEC FUEL softkey 6-6, 6-11 Default power-on settings 5-4 Density Altitude 7-87 Departure 7-57 Load 2-36, 7-44 Procedures 7-67 Remove 2-38, 7-47 Select 2-41, 7-44 Departure timer 7-89 DFLTS softkey 2-5–2-7 DFLT MAP key 1-8 Dilution of Precision 7-92 Direct-to key 1-7, 2-27 Direct-to navigation 2-32, 7-34 Cancel 7-38 Dir
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INDEX J Jeppesen ii, A-1 Joystick 1-7 L L-3 SKYWATCH TAS 8-9–8-10 L-3 Stormscope Weather 8-2–8-6 Land data 7-15 Land group options 7-24 Lean Page 6-1 LEAN softkey 6-4 LEGEND softkey 8-19 Lightning 2-5, 8-2–8-6, 8-13–8-15, 8-27 Line Replaceable Unit (LRU) 1-1–1-5 Liquid crystal displays 7-1 Load indicator 6-8 Long-range planning 8-1 Long range tanks 6-3 LRU Information Window 8-27 LTNG softkey 8-17 M Magnetic Variation 7-75 Magnetometer 1-2, 1-13 Manifold pressure 6-2 Manual sequencing C-2 Manual squelch (
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INDEX R STANDBY softkey 8-9 STAR softkey 7-68 STBY softkey 2-6–2-8, 4-3 STD BARO softkey 2-5–2-7 Stereo Headsets 5-2 Stormscope, L-3 8-2–8-6 Stormscope Page 8-5–8-6 Storm Warnings 8-20 Stuck microphone 3-7 SUSP 2-21 Symbols F-1 System annunciations 9-7–9-9 System message advisories 9-10–9-17 SYSTEM softkey 7-2 System time box 2-24 System time format 7-97 Radar coverage 8-17 Radio selection 3-1 RADIO softkey 8-23 Radio status indications 3-1 Radio tuning window 2-20 RAIM C-1 Recently used VORs 3-16 Recorde
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INDEX VLOC receiver 7-60 Voice alerts 9-4, 9-6 VOL/PUSH ID knob 3-3, 3-8 VOL/PUSH SQ knob 3-3, 3-5 Voltmeter 6-2, 6-10 Volume 5-5 Volume/squelch control 5-8 VOR 3-2, 3-8, 3-16, 3-18 VOR/ILS approach, frequency activation 3-14 VOR list 7-76 VOR Page Menu 7-76 Vspeeds 2-9, 2-30 X XM Information Page 8-23 XM LTNG softkey 2-5, 8-13 XM Radio Interface Softkeys 8-24 XM Radio Page 8-24 XM Satellite Radio 8-23 XPDR softkey 2-6–2-8, 4-1, 4-3, 4-4, 4-5 Z Zoom range 2-25, 8-4 W WARN 2-21 WARNING 9-2 Warning, altitu
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INDEX This page intentionally left blank I-6 Garmin G1000 Pilot’s Guide for the Diamond DA40 190-00592-00 Rev.
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Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p: 913.397.8200 f: 913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p: 503.391.3411 f: 503.364.2138 Garmin (Europe) Ltd. Unit 5, The Quadrangle Abbey Park Industrial Estate Romsey, SO51 9DL, U.K. p: 44/0870.8501241 f: 44/0870.8501251 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com © 2005 Garmin Ltd.