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Two types of lubricating systems for reciprocating aircraft engines are.
The lubrication is distributed to the parts of a reciprocating engine by these three methods.
The main disadvantages of a wet-sump engine are:
- Size is limited
- cooling is difficult
- temperature is high
What two markings must be on the oil filler cap?
Oil tanks used on engines equipped with hydromatic propellers will feed the pressure pump from a standpipe leaving a reserve of oil for _____ _____ .
A gear type oil pump is a _____ dispacement pump.
Constant-displacment oil pumps ___ require a relief valve to control their output pressure.
The 2 types of oil filter systems are
In the ______ filter system only a portion of the oil is filtered each time it circulates
the most popular filter in common use for general aviation aircraft is the disposible ____ filter
The CUNO filter is an ____ filteration type oil filter.
The _____ _____ valve determines which of the two possible paths the oil will take through a cooler.
Whe the oil is cold, it flows _____ the core of the oil cooler.
____ _____ is a system installed on some reciprocating engines to aid in cold weathers starting by introducing fuel into the oil system prior to shutdown.
Oil pressure is measured at the ______ of the engine driven oil pump.
The main contaminents found in used engine oil are:
- Metallic Particles
Oil coolers are normally removed and thoroughly cleaned and inspected at _____ _____.
The oil pressure on engines using an adjustible oil pressure relief may be increased by turning the adjustment screw _____.
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