Lighting Systems; Pitot Static System And Instruments; Airspeed Indicator; Aural Speed Warning - Cessna T206H Flight Manual

SOLOY TURBINE PAC
POHS CESSNA T206H/206H
Before connecting an external power source confirm
that the battery and avionics switches are in the off
position.

LIGHTING SYSTEMS

CABIN HEATING, VENTILATING AND DEFROSTING
– No Change
SYSTEM

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
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
F.A.A. Approved
NOTE
– No Change
or until horn is no longer activated.
MO
7-25
SECTION 7
AIRPLANE & SYSTEMS
DESCRIPTION
May 23, 2003