SOLOY TURBINE PAC
SECTION 7
POHS CESSNA T206H/206H
AIRPLANE & SYSTEMS
DESCRIPTION
7-10
F.A.A. Approved
May 23, 2003
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.
Oil from the cooler is then circulated back to the integral tank. The
propeller reduction gearbox oil is routed from the tank to the gearbox
oil pump then through a filter in the gearbox. The oil is retrieved from
the gearbox by a scavenge pump, and passes by an oil chip detector
through a filter and back into the integral tank. Engine oil also
operates the propeller pitch mechanism and the engine torquemeter
system.
The total lubrication system capacity is 9 U.S. quarts. The oil tank
capacity is 6 U.S. quarts with 4 through 6 quarts marked on the
dipstick for measuring purposes. Recommended oils and oil servicing
procedures are covered in Section 8 of this handbook.
IGNITION SYSTEM
The ignition system consists of a start motor switch, ignition exciter,
spark igniter lead and spark igniter. When installed, a start counter is
mounted on the engine gearbox adjacent to the ignition exciter. The
counter records the total starts on the engine. This is an optional
installation.
The three-position start motor switch located on the left side of the
switch and control panel is placarded START, OFF and MOTOR. The
switch automatically returns to the center (OFF) position when
released. Electrical power will continuously be applied to the ignition
exciter when the start motor switch is in the START position and the
battery switch is on, and will be terminated when the switch is
released, manually placed to the MOTOR position, or if the battery
switch is turned off.
UNCONTROLLED
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