Garmin Cessna Caravan G1000 Руководство пилота - Страница 6

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Garmin Cessna Caravan G1000 Руководство пилота

The G1000 integrated avionics system consolidates all communication, navigation, surveillance, primary ﬂ ight instrumentation,

engine indication system and annunciations on two (or three) liquid crystal displays (LCDs) and one (or two) audio panels. All of

the components of the G1000 system are line-replaceable units (LRUs). This modular approach allows the various components to be

mounted either behind each of the displays, or in remote locations in the aircraft, based upon the needs of the aircraft manufacturer.

Figure 1 is a sample system schematic that shows the G1000 components used in a typical single-engine, GA aircraft.

NOTE: Autopilot interfaces are not shown, for they vary from aircraft to aircraft.

GDU 1040

No. 1 GIA 63

Integrated Avionics Unit

System Inegration Processors

I/O Processors

VHF COM

VHF NAV/LOC

GPS

Glideslope

G1000 SYSTEM OVERVIEW

High-Speed Data Bus (Ethernet)

GMA 1347

Audio Panel

Reversionary

Control

Vertical Speed

G P S O u t p u t

Magnetometer

Transponder

Engine/Airframe

Figure 1 G1000 System

Garmin G1000 Guide for Designated Pilot Examiners & Certiﬁed Flight Instructors

Reversionary

Control

GDC 74A

Air Data

Computer

OAT

Airspeed

Altitude

GRS 77

AHRS

Attitude

Rate of Turn

Slip/Skid

GMU 44

Heading

GTX 32

or GTX 33

GEA 71

Unit