Card Set Information
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:
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 _____.