SOLOY TURBINE PAC
SECTION 7
POHS CESSNA U/TU 206G
AIRPLANE & SYSTEMS
DESCRIPTION
7-15
F.A.A. Approved
October 4, 2005
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.
NEW ENGINE BREAK-IN AND OPERATION
There are no specific break-in procedures required for the SOLOY
TURBINE PAC turboprop engine. The engine may be safely operated
through the normal ranges authorized by the manufacturer at the time
of delivery of your airplane.
ENGINE OIL SYSTEM
Engine oil, contained in an integral tank of the SOLOY TURBINE PAC,
cools as well as lubricates the system. Oil is drawn from the tank
through a pickup line to the engine-driven oil pump. Oil from the pump
passes by an oil chip detector and is routed through a pressure screen
to the engine. Then, from the engine past an oil chip detector, the oil is
circulated through an external oil filter to a thermostatically controlled
oil cooler.
UNCONTROLLED
COPY