SOLOY TURBINE PAC
SECTION 7
POHS CESSNA T206H/206H
AIRPLANE & SYSTEMS
DESCRIPTION
7-25
F.A.A. Approved
May 23, 2003
NOTE
Before connecting an external power source confirm
that the battery and avionics switches are in the off
position.
LIGHTING SYSTEMS
– No Change
CABIN HEATING, VENTILATING AND DEFROSTING
SYSTEM
– No Change
PITOT STATIC SYSTEM AND INSTRUMENTS
AIRSPEED INDICATOR
The airspeed indicator is calibrated in knots. Limitation and range
markings include the white arc (40 to 96 knots), with a step at (49
knots), and a red line (149 knots).
AURAL SPEED WARNING HORN
This aircraft is equipped with an Aural Speed Warning Horn that
activates when the airspeed indicator is approximately 5 knots
above Vmo. If an aural speed warning is activated, reduce speed
to 30 knots below V
MO
or until horn is no longer activated.
VERTICAL SPEED INDICATOR
– No Change
ALTIMETER
– No Change
VACUUM SYSTEM AND INSTRUMENTS
ATTITUDE INDICATOR
– No Change
DIRECTIONAL INDICATOR
– No Change
VACUUM GAUGE
The vacuum gauge is located on the lower left corner of the
instrument panel. It is calibrated in inches of mercury and
indicates vacuum air available for operation of the attitude and
directional indicators. During operation at altitudes below 15,000
UNCONTROLLED
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