190-00820-11 Rev. A
Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin
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 GARMIN LINE REPLACEABLE UNITS (LRU)
•
GDU 1240A-30/1040A-30
(1) – This unit is configured as a PFD that features a 12 or 10.4-inch LCD with 1024
x 768 resolution. The unit installed on the left/pilot side is designated as the PFD. This unit communicates
with the GDU 1240A-20/1040A-20 (MFD), and with the on-side GIA 63W Integrated Avionics Unit through a
High-Speed Data Bus (HSDB) connection.
•
GDU 1240A-20/1040A-20
(1) – This unit is configured as a MFD that features a 12 or 10.4-inch LCD with 1024
x 768 resolution. The unit installed on the right/copilot side is designated as MFD. This unit communicates
with the GDU 1240A-30/1040A-30 (PFD), and with the on-side GIA 63W Integrated Avionics Unit through a
High-Speed Data Bus (HSDB) connection.
•
GIA 63W
(2) – The Integrated Avionics Units (IAU) function as the main communication hub, linking all
LRUs with the PFD. Each GIA 63W contains a GPS Satellite-Based Augmentation System (SBAS) receiver,
VHF COM/NAV/GS receivers, a flight director (FD; if the Garmin AFCS is installed) and system integration
microprocessors. Each GIA 63W is paired with the on-side display via an HSDB connection. The GIA 63Ws
are not paired and do not communicate with each other directly.
