SECTION 7 CESSNA
AIRPLANE AND SYSTEMS
DESCRIP'fION MODEL 182T NAV Ill
STANDARD AVIONICS
The Garmin GlOOO Avionics System is an integrated flight control
and navigation system.
The system combines primary flight
instruments, communications, aircraft system information and
navigational information all displayed on two color displays. The
GI000 system consists of the following pieces of equipment:
GDU 1040 Color Display
-
Two identical units are mounted on the
instrument panel. One, located in front of the pilot, is configured as
a Primary Flight Display, or PFD. A second panel, located to the
right, is configured as a Multi-Function Display, or MFD.
'The PFD displays roll and pitch information, heading and course
navigation information, plus altitude, airspeed and vertical speed
information to the pilot.
The PFD also controls and displays all
communication and navigation frequencies as well as displaying
warninglstatus annunciations of aircraft systems.
The MFD displays a large scalable, moving map that corresponds to
the airplane's current location. Data from other components of the
system can be over laid on this map. Location and direction of
movement of nearby aircraft, lightning and weather information can
all be displayed on the MFD. The MFD is also the principle display
of all of the engine parameters and fuel information.
A Reversionary Mode places the flight information and basic engine
information on both the PFD and the MFD. This feature allows the
pilot full access to all necessary information should either of the
display screens malfunction.
GMA 1347 Audio Panel
-
The audio panel for the GlOOO system
integrates all of the communication
&
navigation digital audio
signals, intercom system and marker beacon controls in one unit. It
is installed on the instrument panel between the PFD and the MFD.
The GMA 1347 also controls the Reversionary Mode for the PFD
and MFD.
NOTE
Use of the COM 112 function is not approved.
(Continued Next Page)
7-66 U.S.
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