System overview – Garmin G1000 Mooney M20TN User Manual

Page 19

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190-00647-02 Rev. A

Garmin G1000 Pilot’s Guide for the Mooney M20M/M20R/M20TN

5

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

Figure 1-1 Basic G1000 System Block Diagram

GSA 81

Roll Servo

Autopilot Calculations

(optional)

GSA 81

Pitch Servo

Autopilot Calculations

(optional)

GSA 81

Pitch Trim Servo

Autopilot Calculations

(optional)

No. 1 GIA 63W

Integrated Avionics Unit


System Inegration Processors

I/O Processors

VHF COM

VHF NAV/LOC

GPS

Glideslope

Flight Director (with AFCS option)

No. 2 GIA 63W

Integrated Avionics Unit


System Integration Processors

I/O Processors

VHF COM

VHF NAV/LOC

GPS

Glideslope

GTX 33

Transponder

High-Speed Data Bus (Ethernet)

Reversionary

Control

GEA 71

Engine/Airframe

Unit

GDC 74A

Air Data

Computer

OAT

Airspeed

Altitude

Vertical Speed

GRS 77

AHRS


Attitude

Rate of Turn

Slip/Skid

GMU 44

Magnetometer

Heading

GPS Output

GPS Output

Reversionary

Control

GMA 1347

Audio Panel

GDU 1040 (PFD)

GDU 1040 or

GDU 1042/1044 (MFD)

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