1 line replaceable units, System overview – Garmin G950 Tecnam 2006T User Manual

Page 14

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Garmin G950 Pilot’s Guide for the Tecnam P2006T

190-01146-00 Rev. A

2

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

1.1 LINE REPLACEAbLE UNITS

• GDU 1040 (2) – The left-hand GDU is configured as a Primary Flight Display (PFD) and the right-hand GDU

as a Multi Function Display (MFD). Both feature 10.4-inch LCD screens with 1024 x 768 resolution. The
displays communicate with each other through a High-Speed Data Bus (HSDB) Ethernet connection. Each
display is also paired with an Ethernet connection to an IAU.

GMA 1347

(1) – The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio,

intercom, and marker beacon controls, and is installed between the displays. This unit also provides manual
control of display reversionary mode (red

DISPLAY BACKUP

Button; see Section 1.5, System Operation) and

communicates with both IAUs using an RS-232 digital interface.

• GIA 63W (2) – The Integrated Avionics Units (IAU) function as the main communication hubs, linking all

LRUs with the on-side display. Each IAU contains a GPS WAAS receiver, VHF COM/NAV/GS receivers, and
system integration microprocessors, and is paired with the on-side display via HSDB connection. The IAUs are
not paired together and do not communicate with each other directly.

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