User manual GARMIN G1000 MOONEY SYSTEMOVERVIEW M20M M20R

[. . . ] G1000 TM system overview for Mooney M20M & M20R Record of Revisions Revision Date of Revision Revision Page Range A 05/16/05 -----Description Initial release. Garmin G1000 System Overview for Mooney M20M & M20R 190-000442-01 Rev. A SYSTEM OVERVIEW 2. 1 SYSTEM DESCRIPTION This document is designed to provide an overview of the G1000 Integrated Cockpit System as installed in Mooney M20M & M20R aircraft. The G1000 system includes the following Line Replaceable Units (LRUs): · · · · · · · · · · GDU 1040 Primary Flight Display (PFD) GDU 1040 Multi Function Display (MFD) GIA 63 Integrated Avionics Units (2) GEA 71 Engine/Airframe Unit GDC 74A Air Data Computer (ADC) GRS 77 Attitude and Heading Reference System (AHRS) GMU 44 Magnetometer GMA 1347 Audio System with integrated Marker Beacon Receiver GTX 33 Mode-S Transponder GDL 69/69A Data Link 2. 2 LINE REPLACEABLE UNITS · GDU 1040 ­ The GDU 1040 features a 10. 4-inch LCD display with 1024 x 768 resolution. The left display is configured as a PFD and the right display is configured as an MFD. [. . . ] Pressing this knob centers the CDI on the currently selected VOR. · (7) Dual COM Knob ­ Tunes the MHz (large knob) and kHz (small knob) standby frequencies for the COM transceiver. Pressing this knob toggles the tuning cursor (cyan box) between the COM1 and COM2 fields. · (8) COM Frequency Toggle Key ­ Toggles the standby and active COM frequencies. Pressing and holding this key for two seconds automatically tunes the emergency frequency (121. 5 MHz) in the active frequency field. · (9) COM VOL/SQ Knob ­ Controls COM audio level. Pressing this knob turns the COM automatic squelch ON and OFF. Audio volume level is shown in the field as a percentage. · (10) Direct-to Key ( ) ­ Allows the user to enter a destination waypoint and establish a direct course to the selected destination (specified by the identifier, chosen from the active route, or taken from the map cursor position). · (11) FPL Key ­ Displays the active Flight Plan Page for creating and editing the active flight plan, or for accessing stored flight plans. · (12) CLR Key (DFLT MAP) ­ Erases information, cancels an entry, or removes page menus. To display the Navigation Map Page immediately, press and hold CLR (MFD only). · (13) Dual FMS Knob ­ 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. When the cursor is ON, data may be entered in the different windows using the small and large knobs. The large knob is used to move the cursor on the page, while the small knob is used to select individual characters for the highlighted cursor location. When the G1000 displays a list that is too long for the display screen, a scroll bar appears along the right side of the display, indicating the availability of additional items within the selected category. Press the FMS/PUSH CRSR knob to activate the cursor and turn the large FMS knob to scroll through the list. · (14) MENU Key ­ Displays a context-sensitive list of options. This list allows the user to access additional features, or to make setting changes that relate to certain pages. 2-8 Garmin G1000 System Overview for Mooney M20M & M20R 190-000442-01 Rev. A SYSTEM OVERVIEW · (15) PROC Key ­ Selects approaches, departures and arrivals from the flight plan. [. . . ] The change to backup paths is completely automated for all LRUs, and no pilot action is required. NOTE: The system alerts the pilot when backup paths are utilized by the LRUs. Refer to the Annunciations and Alerts Pilot's Guide for further information regarding these and other system alerts. Reversionary mode may also be manually activated by the pilot if the system fails to detect a display problem. Reversionary mode is activated manually by pressing the red DISPLAY BACKUP button at the bottom of the GMA 1347. Pressing this button again deactivates reversionary mode. Figure 2. 7. 2 Reversionary Mode (Failed PFD) 190-000442-01 Rev. [. . . ]