190-00595-01 Rev. B
Garmin G1000 Pilot’s Guide for the Beechcraft A36/G36
1
SYSTEM OVERVIEW
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& cNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the G1000 Integrated Flight Deck as installed in the Beechcraft A36/G36
Bonanza. 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 system
consists 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 Marker
Beacon 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 Gearboxes
A 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 flight
director (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system.