190-00595-01 Rev. B Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36 1SYSTEM OVERVIEWSYSTEMOVERVIEW FLIGHTINSTRUMENTS EIS AUDIO PANEL& cNS FLIGHTMANAGEMENT HAZARDAVOIDANCE AFCS ADDITIONALFEATURES APPENDICES INDEXSECTION 1 SYSTEM OVERVIEW1.1 SYSTEM DESCRIPTIONThis section provides an overview of the G1000 Integrated Flight Deck as installed in the Beechcraft A36/G36Bonanza. The G1000 system is an integrated flight control system that presents flight instrumentation, position,navigation, communication, and identification information to the pilot through large-format displays. The systemconsists of the following Line Replaceable Units (LRUs):• GDU 1040 Primary Flight Display (PFD)• GDU 1043/1045 Multi Function Display (MFD)• GIA 63/63W Integrated Avionics Unit• GDC 74A Air Data Computer (ADC)• GEA 71 Engine/Airframe Unit• GRS 77 Attitude and Heading Reference System(AHRS)• GMU 44 Magnetometer• GMA 1347 Audio System with Integrated MarkerBeacon Receiver• GTX 33 Mode S Transponder• GDL 69A Satellite Data Link Receiver• GTP 59 Outside Air Temperature (OAT) Probe• GSA 81 AFCS Servos• GSM 85 Servo GearboxesA top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GSM 85A).NOTE: Refer to the AFCS section for details on the GFC 700 AFCS.In the Beechcraft A36/G36 Bonanza, the GFC 700 Automated Flight Control System (AFCS) provides the flightdirector (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system.
