SOLOY TURBINE PAC SECTION 7
POHS CESSNA T206H/206H AIRPLANE & SYSTEMS
DESCRIPTION
7-9
F.A.A. Approved May 23, 2003
counterbalanced by oil from the lubrication system. The cylinder
oil pressure is quoted to an external connection for use with a
torque indicator that is calibrated in PSI of torque.
PROPELLER RPM INDICATOR (N
P
)
The propeller RPM indicator (N
P
) is a tachometer which indicates
the propeller speed in revolutions per minute. The power turbine
speed (N
2
) can also be determined with the indicator where 18.1
N
P
RPM is equal to 1% N
2
speed.
TOT INDICATOR
The turbine outlet temperature gauge displays the gas
temperature in the gas producer turbine outlet.
N
1
PERCENT RPM INDICATOR
The N
1
RPM indicator indicates the percent of the gas producer
RPM based on a figure of 105% N
1
at 53,519 RPM.
ENGINE OIL PRESSURE INDICATOR
Oil pressure is displayed in pounds per square inch.
ENGINE OIL TEMPERATURE INDICATOR
Oil temperature is measured at the engine oil inlet and is
electrically transmitted and displayed by the indicator in degrees C.
TRANSMISSION OIL PRESSURE INDICATOR
Oil pressure is directly measured and displayed in pounds per
square inch.
FUEL TOTALIZER/TEMPERATURE INDICATOR
The fuel totalizer/temperature indicator displays the flow of fuel to
the engine in pounds per hour, time remaining in hours and
minutes, pounds used, pounds remaining and fuel temperature.
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