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CESSNA
SECTION 2
MODEL 162
AIRPLANE AND SYSTEM DESCRIPTION
GARMIN G300
U.S.
ENGINE
(Continued)
ENGINE LUBRICATION SYSTEM
The engine utilizes a full pressure, wet sump type lubrication system
with aviation grade oil as the lubricant. The capacity of the engine
sump, located on the bottom of the engine, along with the engine oil
filter and oil cooler is 5.5 quarts. Oil is drawn from the sump through a
filter screen on the end of a pickup tube to the engine driven oil pump.
Oil from the pump then passes through a full-flow oil filter, a pressure
relief valve at the rear of the right oil gallery, and an oil cooler before
lubricating engine parts. The oil returns to the sump by gravity. The filter
adapter in the full-flow filter is equipped with a bypass valve which will
cause lubricating oil to bypass the filter in the event the filter becomes
plugged, or the oil temperature is extremely cold.
An oil dipstick/filler tube is located at the left rear of the engine case.
The oil dipstick/filler tube is accessed through a door located on the left
side of the engine cowling. The engine should not be operated on less
than 3.5 quarts of oil. For extended flight, fill to 5.0 quarts (dipstick
indication only). For engine oil grade and specifications, refer to
Section 8 of this POH.
IGNITION AND STARTER SYSTEM
Engine ignition is provided by two engine driven magnetos, and two
spark plugs in each cylinder. The left magneto fires the lower left and
lower right spark plugs, and the right magneto fires the upper left and
upper right spark plugs. Normal operation is conducted with both
magnetos due to the more complete burning of the fuel/air mixture with
dual ignition.
Ignition and starter operation is controlled by a rotary-type switch
located on the left instrument panel. The MAGNETOS switch is labeled
clockwise, OFF, R, L, BOTH, and START. The engine should be
operated on both magnetos (BOTH position) except for magneto
checks. The R and L positions are for checking purposes and
emergency use only. When the MAGNETOS switch is rotated to the
spring-loaded START position, with the MASTER switch in the ON
position, the starter contactor is closed and the starter, now energized,
will crank the engine. When the switch is released, it will automatically
return to the BOTH position.
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162PHUS-00
2-13
Содержание 162 SKYLANE
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