Chapter9b

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:

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:

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 _____.