190-00663-00 Rev. A
Garmin G1000 Pilot’s Guide for the Hawker Beechcraft C90A/GT
1-1
SYSTEM OVERVIEW
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section provides an overview of the G1000 Integrated Flight Deck as installed in the Hawker Beechcraft
C90A/GT. 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 1040A
Primary Flight Display (PFD)
•
GDU 1500
Multi Function Display (MFD)
•
GIA 63W
Integrated Avionics Unit
•
GDC 74B
Air Data Computer (ADC)
•
GEA 71
Engine/Airframe Unit
•
GRS 77
Attitude and Heading Reference System
(AHRS)
•
GMU 44
Magnetometer
•
GMA 1347D
Dual Audio System with Integrated
Marker Beacon Receiver
•
GTX 33
Mode S Transponder
•
GDL 69A
Satellite Data Link Receiver
•
GWX 68
Weather Radar
•
GCU 475
MFD Control Unit
•
GMC 710
AFCS Control Unit
•
GTP 59
Outside Air Temperature (OAT) Probe
•
GSA 80
and
GSA 81
AFCS Servos
•
GSM 85A
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 Hawker Beechcraft C90A/GT, the GFC 700 Automated Flight Control System (AFCS) provides the flight
director (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system.
Summary of Contents for G1000:Beechcraft Baron 58/G58
Page 1: ...Hawker Beechcraft C90A GT...
