Garmin Cessna Caravan G1000 Manuel du pilote - Page 7

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The main components of the G1000 system are the two GDU 1040 displays used for the Primary Flight Display (PFD) and the Multi

Function Display (MFD), and the two GIA 63 Integrated Avionics Units (IAUs). These components are interfaced with each other via

a proprietary Ethernet-based, high-speed digital databus system. All other components, such as the Attitude and Heading Reference

System (AHRS), Air Data Computer (ADC), transponder and Engine/Airframe Interface units, use combinations of RS-232, ARINC 429

and RS-485 interfaces.

Both GDU 1040 displays are identical in hardware. The aircraft wiring harness determines whether the display functions as a PFD

or an MFD (see Figure 2). A conﬁguration module within the PFD connector contains aircraft-speciﬁc backup conﬁguration data.

Failure Mode(s)

If one display fails, the primary ﬂight instruments and Engine Indication System (EIS) are displayed on the remaining screen. No

moving map is presented in this mode (see Figure 3). This operating mode is called "reversionary mode" and may be either detected

automatically by the system, or initiated manually via the red DISPLAY BACKUP button located on the lower portion of the audio

panel.

190-00368-02 Rev. A

G1000 SYSTEM COMPONENTS

Garmin G1000 Guide for Designated Pilot Examiners & Certiﬁed Flight Instructors