Garmin G1000 PDAs & Smartphones User Manual


 
190-00498-07 Rev. A
Garmin G1000 Pilot’s Guide for Cessna Nav III
1
SYSTEM OVERVIEW
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
SECTION 1 SYSTEM OVERVIEW
1.1 SYSTEM DESCRIPTION
This section is designed to provide an overview of the G1000 Integrated Flight Deck as installed in Cessna Nav
III aircraft, which include the Cessna 172R, 172S, the normally aspirated Cessna 182 (182), the turbocharged
Cessna 182 (T182), the normally aspirated Cessna 206 (206), and the turbocharged Cessna 206 (T206).
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 1040/1044B
Primary Flight Display (PFD)
•
GDU 1040/1044B
Multi Function Display (MFD)
•
GIA 63/63W
Integrated Avionics Unit (IAU)
•
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
•
GTS 800
Traffic Avoidance System (optional)
•
GDL 90
ADS-B/FIS-B Data Link Transceiver (optional)
•
GSA 81
AFCS Servos
•
GSM 85
Servo Gearboxs
A top-level G1000 system block diagram is shown in Figure 1-1. See Figure 1-2 for optional/additional
equipment.
NOTE: Refer to the AFCS section for details on the GFC 700 AFCS.
The GFC 700 Automated Flight Control System (AFCS) provides the flight director (FD) and autopilot (AP)
functions of the G1000 system.