BasicAero, PPL Flashcards
Whr may an a/c’s operating limitations be found?
In the current, FAA-approved flight manual, approved manual material, marking, and placards. or any combination thereof.
The operating principle of float-type carturetors is based on the
difference in air pressure at the venturi tgroat and the air inlet.
The basic purpose of adjusting the fuel/air mixture at altitude is to
decrease the fuel flow in order to compensate for decreased air density.
During tge run-up at a high-elevation airport, a pilot notes a slight engine roughtness that is not affected by the magneto check but grows worse during the carburetor heat check. Under these circunstances, what would be the most logical initial action?
Check the rusults obtained with a leaner setting of the mixture.
While cruising at 9500feet MSL, the fuel/air mixture is properly adjusted. What will occur if a descent to 4500feet MSL is made without readjusting the mixture?
The fuel/air mixture may becone excessively lean.
Excessively high engine temp will
cause loss pwr, excessive oil consumption
If the engine oil temp and cylinder head temp gauges have exceeded their normal operating range, the pilot may have been operating with
too much pwr and with the mixture set too lean
One purpose of the dual ignition system on an a/c engine is to provide for
Improved engine performance
On a/c equipped with fuel pumps, when is the aux electric driven pump used?
In the event engine-driven fuel pump fails.
The presence of carburetor ice in an a/c equipped witg a fixed-pitch propeller can be verified by applying carburetor heat and noting
a decrease in RPM and then a gradual increase in RPM
With regard to carburetor ice, float-type carburetor systems in comparison to fuel injection systems are generally considered to be
more susceptible to icing
If the grade of fuel used in an a/c engine is lower than specified for engine, it will mose likely cause
detonation
Detonation occurs in a reciprocating a/c engine when
the unburned charge in the cylinders explodes instead of burning normally
If a pilot suspects that engine (wt a fixed-pitch propeller) is detonation during climb-out after t/o, the initial corrective action to take would to
lower the nose slightly to increase a/s
Which condition is most favorable to the development of carburetor icing?
Temp btw 20 and 70 degree F and high humidity