Garmin G1000 Mooney M20TN - Manual (Page 12)

190-00647-01 Rev. B Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN 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
NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the GFC 700 AFCS.
The G1000 is an integrated flight deck system that presents flight instrumentation, position, navigation,
communication, and identification information to the pilot using flat-panel color displays. The system consists of
the following Line Replaceable Units (LRUs):
• GDU 1040 Primary Flight Display (PFD)
• GDU 1042/1044 Multi Function Display (MFD)
• GMA 1347 Audio Panel with Integrated Marker
Beacon Receiver
• GIA 63(W) Integrated Avionics Units (IAU)
• GDC 74A Air Data Computer (ADC)
• GEA 71 Engine/Airframe Unit
• GTX 33 Mode S Transponder
• GRS 77 Attitude and Heading Reference System
(AHRS)
• GMU 44 Magnetometer
• GDL 69A Data Link Receiver
• GSA 81 AFCS Servos
• GSM 85 Servo Gearbox
Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are shown in Figure 1-2.
The Mooney M20M/M20R/M20TN is equipped with a GFC 700 Automated Flight Control System (AFCS),
providing flight director (FD), autopilot (AP), and manual electric trim (MET) functions of the G1000 System.