User manual GARMIN G1000 BEECHCRAFTA36 G36 SYSTEMOVERVIEW

[. . . ] G1000 TM System Overview for the Beechcraft A36/G36 Record of Revisions Revision Date of Revision Revision Page Range A 7/19/05 ----------Description Initial release Garmin G1000 System Overview for the Beechcraft A36/G36 190-00571-00 Rev. A SYSTEM OVERVIEW 2. 1 INTRODUCTION This System Overview Pilot's Guide provides a basic description of the G1000 System as it pertains to the Beechcraft A36/G36. The description includes the Garmin Automatic Flight Control System (AFCS). 2. 2 SYSTEM DESCRIPTION This section gives a brief description of the G1000 System. Refer to the Pilot's Guide Appendices for LRU specifications. High-Speed Data Bus (Ethernet) Reversionary Control Reversionary Control No. [. . . ] · (7) CRS/BARO Knob ­ The large knob sets the altimeter barometric pressure and the small knob adjusts the course. The course is only adjustable when the HSI is in VOR1, VOR2, or OBS/SUSP mode. Pressing this knob centers the CDI on the currently selected VOR. · (8) 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. · (9) 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. · (11) 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). · (12) FPL Key ­ Displays the active Flight Plan Page for creating and editing the active flight plan, or for accessing stored flight plans. · (13) 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). 2-6 Garmin G1000 System Overview for the Beechcraft A36/G36 190-00571-00 Rev. A SYSTEM OVERVIEW · (14) 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. 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. · (15) 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. · (16) PROC Key ­ Selects approaches, departures and arrivals from the flight plan. If a flight plan is used, available procedures for the departure and/or arrival airport are automatically suggested. If a flight plan is not used, the desired airport and the desired procedure may be selected. This key selects IFR departure procedures (DPs), arrival procedures (STARs) and approaches (IAPs) from the database and loads them into the active flight plan. [. . . ] In reversionary mode, all important flight information is shown on the remaining display. An example of reversionary mode entry due to a failed PFD is shown in Figure 2. 7. 2. If a display fails, the GIA 63-GDU 1040 Ethernet interface is cut off. Thus, the GIA can no longer communicate with the remaining display (refer to Figure 2. 2. 1), and the NAV and COM functions provided to the failed display by the GIA are flagged as invalid on the remaining display. [. . . ]