2.13 Carburetor Icing Flashcards
with regard to carburetor ice, float-type carburetor systems in comparison to fuel injection systems are generally considered to be
more susceptible to icing
which condition is most favorable to the development of carburetor icing
temperature between 20° F and 70° F and high humidity
the possibility of carburetor ice exists even when the ambient air temperature is as
High at 70° F and the relative humidity is high
if an aircraft is equipped with a fixed pitch propeller and a float type carburetor, the first indication of carburetor ice would most likely be
decrease/loss of RPM
the operating principle of float type carburetors is based on
difference in air pressure at the venturi throat and the air inlet
the presence of carburetor ice in an aircraft equipped with fixed pitch propeller can be verified by applying carburetor heat and noting
a decrease in RPM and then a gradual increase in RPM