Cessna skylance tc T182T, Информационное руководство

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CESSNA SECTION 7
MODEL T182T NAV III AIRPLANE AND SYSTEM DESCRIPTION
GFC 700 AFCS
U.S.
STANDARD AVIONICS
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AIR DATA COMPUTER (GDC)
The Air Data Computer (ADC) compiles information from the airplane's
pitot/static system. The ADC unit is mounted behind the instrument
panel, just forward of the MFD. An outside air temperature probe,
mounted on top of the cabin, is connected to the ADC. The ADC
calculates pressure altitude, airspeed, true airspeed, vertical speed and
outside air temperature.
ENGINE MONITOR (GEA)
The Engine Monitor is responsible for receiving and processing the
signals from all of the engine and airframe sensors. It is connected to
all of the CHT measuring sensors, EGT sensors, manifold pressure,
RPM, fuel flow and to the fuel gauging system. This unit transmits this
information to the engine display computers.
TRANSPONDER (GTX)
The full-featured Mode S transponder provides Mode A, C and S
functions. Control and operation of the transponder is accomplished
using the PFD. The transponder unit is mounted in the tailcone avionics
racks.
XM WEATHER AND RADIO DATA LINK (GDL)
The XM weather and radio data link provides weather information and
digital audio entertainment in the cockpit. The unit is mounted behind
the instrument panel, just forward of the MFD. This unit communicates
with the MFD on the high-speed data bus. XM weather and XM radio
operate in the S-band frequency range to provide continuous uplink
capabilities at any altitude throughout North America. A subscription to
the XM satellite radio service is required for the XM weather and radio
data link to be used.
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T182TPHBUS-00 7-85