N 1 Percent Rpm Indicator; Engine Oil Pressure Indicator; Engine Oil Temperature Indicator; Transmission Oil Pressure Indicator - Cessna U206G STATIONAIR Pilot Operating Handbook

SOLOY TURBINE PAC
POHS CESSNA U/TU 206G
N PERCENT RPM INDICATOR
1
The N RPM indicator indicates the percent of the gas producer
1
RPM based on a figure of 105% N

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.
F.A.A. Approved
AIRPLANE & SYSTEMS
at 53,519 RPM.
1
7-15
SECTION 7
DESCRIPTION
October 4, 2005