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.