User manual GARMIN G1000: TIGER AG-5B PILOT'S GUIDE -- (PART 1 OF 2) REV. A, JUL, 2005

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   GARMIN G1000: TIGER AG-5B PILOT'S GUIDE -- (PART 2 OF 2) REV. A, JUL, 2005 (6789 ko)

Manual abstract: user guide GARMIN G1000: TIGER AG-5BPILOT'S GUIDE -- (PART 1 OF 2) REV. A, JUL, 2005

Detailed instructions for use are in the User's Guide.

[. . . ] The PFD provides increased situational awareness by replacing the traditional "six pack" of instruments in the pilot's panel with an easy-to-scan display that provides a large horizon, airspeed, attitude, altitude, vertical speed, navigation, communication, annunciation, terrain, traffic and lightning information. The PFD also controls the operation of the transponder, the selection of NAV/COM frequencies, audio volume and many navigation features. The operation of these features is explained in other supporting pilot's guide documentation. The G1000 system controls were designed so that, regardless of which seat the pilot is flying from, the aircraft can be flown with one hand and the controls manipulated by the other hand. WARNING: In the event that the airspeed, attitude, altitude, or heading indications become unusable, please refer to the backup instruments. The PFD displays the following: · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Navigation Frequency Window Navigation Status Bar Communication Frequency Window Airspeed Indicator True Airspeed Box Attitude Indicator Slip/Skid Indicator Horizontal Situation Indicator Turn Rate Indicator Bearing Pointers DME Information Window BRG1 Information Window BRG2 Information Window Radio Tuning Window (ADF/DME) Altimeter Altitude Reference Box Barometric Setting Box Vertical Deviation/Glideslope Indicator Marker Beacon Receiver Annunciations Vertical Speed Indicator Alerts Window Annunciation Window System Time Box Transponder Status Bar Outside Air Temperature Box Inset Map Direct-to Window Flight Plan Window Procedures Window Timer/References Window Nearest Airports Window 190-00443-01 Rev. [. . . ] The Time Offset (Time Zone) represents the number of hours plus or minus UTC (refer to the Multi Function Display Pilot's Guide). Figure 3. 6. 2 System Time Box Figure 3. 6. 3 Traffic Annunciation 190-00443-01 Rev. A Garmin G1000 PFD Pilot's Guide for Mooney M20M & M20R 3-29 SUPPLEMENTAL FLIGHT DATA INSET MAP The Inset Map is a smaller version of the Navigation Map Page on the MFD. It appears in the lower left corner of the PFD and is displayed by pressing the INSET softkey. The map disappears from the PFD anytime pitch is greater than +30° and less than ­20°, or when a 65° bank angle is reached. The direct-to function is not available from the Inset Map. The fuel reserve rings are enabled and disabled from the MFD only. The Inset Map displays the following information: NOTE: The map orientation is always the same as that for the Navigation Map Page on the MFD. The following Inset Map operations can be performed and are independent of the MFD: · · · · · · · Change the zoom range Change the declutter level Enable/disable traffic data Enable/disable topo data Enable/disable terrain data Enable/disable weather information (optional) Pan Map 1 2 8 3 4 1 2 3 4 5 6 7 8 9 7 6 5 9 · Moving map with orientation references ­ North Up ­ Track Up ­ DTK Up ­ HDG Up · Zoom range legend · Declutter levels (3) · Aircraft icon · Traffic data · Topo data · Terrain data · Weather information (optional) · Enabled map features · Active navigation route · Track vector · Fuel ring (reserve) NOTE: Map orientation and other map features are enabled on the MFD (refer to the Multi Function Display Pilot's Guide). NOTE: Refer to the Multi Function Display Pilot's Guide for a detailed explanation of the declutter levels. 3-30 Wind Vector NAV Compass Range NAV Compass Traffic Icon and Scale Map Range Terrain Icon Active Navigation Route Track Vector Map Orientation Figure 3. 6. 4 Inset Map Garmin G1000 PFD Pilot's Guide for Mooney M20M & M20R 190-00443-01 Rev. A SUPPLEMENTAL FLIGHT DATA To change the zoom range: 1. Turn the joystick clockwise to increase or counterclockwise to decrease the range. Zoom ranges from 500 feet to 2, 000 nautical miles. This option list allows the pilot to access additional features or make setting changes which specifically relate to the currently displayed window. Some menus provide access to additional sub-menus that are in turn used to view, edit, select and review options. Once the Page Menu window is displayed, turn the FMS knob to scroll through a list of available options (a scroll bar always appears to the right of the window when the option list is longer than the window) and press the ENT key to select the desired option. The CLR key may be pressed to remove the menu and cancel the operation. Pressing the FMS knob also removes the displayed menu. To pan the map: NOTE: The joystick on the PFD operates independently from the one on the MFD. 1. 2. 3. Push in the joystick to display the panning pointer. This allows the pilot to move the map beyond its current limits without adjusting the range. Push in and move the joystick to pan the map Figure 3. 6. 5 Page Menu ­ No Options With NRST Window Displayed in the general direction of the desired location. When the pointer is placed on an object, the name of the object is highlighted for approximately 4 seconds (even if the name was not originally displayed on the map). This feature applies to everything displayed on the map except for route lines. Push in the joystick again to cancel the panning function and return to the present position on Figure 3. 6. 6 Page Menu ­ Options With FPL Window Displayed the map. NOTE: The airspace boundary stays highlighted for approximately 4 seconds before returning to normal shading. NOTE: Pressing the softkeys does not display a menu or sub-menu. 3-32 Garmin G1000 PFD Pilot's Guide for Mooney M20M & M20R 190-00443-01 Rev. [. . . ] A Garmin G1000 PFD Pilot's Guide for Mooney M20M & M20R 3-47 SUPPLEMENTAL FLIGHT DATA This page intentionally left blank. 3-48 Garmin G1000 PFD Pilot's Guide for Mooney M20M & M20R 190-00443-01 Rev. A REVERSIONARY MODE 3. 7 REVERSIONARY MODE The PFD is designed to enter 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 Pilot's Guide). In reversionary mode, the CDUs are re-configured to present the PFD symbology together with the engine parameters (engine parameters are incorporated on the left side of the display). Transition for the pilot is straightforward since PFD parameters are presented in the same format as that prior to the re-configuration. [. . . ]

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