The FAA
Aviation Mechanic - Powerplant
test bank contains questions pertaining to
Propellers
. The following list contains only a relatively small percentage of the pertinent
questions. Our software, which you are free to download now at no cost, will
generally contain a much more complete set of questions associated with this
test bank. This list is intended only to familiarize you in a general way with
the questions of the
Aviation Mechanic - Powerplant
test bank.
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That said, while the following questions are intended
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Aviation Mechanic - Powerplant
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Sample Questions
from the FAA
Aviation Mechanic - Powerplant
Test Bank |
- Propeller fluid anti icing systems generally use which of the following?
- Proper operation of electric deicing boots on individual propeller blades may best be determined by
- What type of imbalance will cause a two blade propeller to have a persistent tendency to come to rest in a horizontal position (with the blades parallel to the ground) while being checked on a propeller balancing beam?
- Apparent engine roughness is often a result of propeller unbalance. The effect of an unbalanced propeller will usually be
- During engine operation at speeds lower than those for which the constant speed propeller control can govern in the INCREASE RPM position, the propeller will
- When the centrifugal force acting on the propeller governor flyweights overcomes the tension on the speeder spring, a propeller is in what speed condition?
- Propellers exposed to salt spray should be flushed with
- The actual distance a propeller moves forward through the air during one revolution is known as the
- Why is a constant speed counterweight propeller normally placed in full HIGH PITCH position before the engine is stopped?
- Which of the following is identified as the cambered or curved side of a propeller blade, corresponding to the upper surface of a wing airfoil section?
- The purpose of permanently sealing and partially filling some models of McCauley propeller hubs with dyed oil is to
- Inspection of propeller blades by dye-penetrant inspection is accomplished to detect
- Most engine propeller combinations have one or more critical ranges within which continuous operation is not permitted. Critical ranges are established to avoid
- The purpose of a three way propeller valve is to
- Geometric pitch of a propeller is defined as the
- What are the rotational speed and blade pitch angle requirements of a constant speed propeller during takeoff?
- Constant-speed non-feathering McCauley, Hartzell, and other propellers of similar design without counterweights increase pitch angle using
- What normally prevents a Hartzell Compact propeller from going to feather when the engine is shut down on the ground?
- How is the oil pressure delivery on a hydromatic propeller normally stopped after the blades have reached their full feathered position?
- On aircraft equipped with hydraulically operated constant speed propellers, all ignition and magneto checking is done with the propeller in which position?
- What is the basic purpose of the three small holes (No. 60 drill) in the tipping of wood propeller blades?
- If a flanged propeller shaft has dowel pins
- Generally, unless otherwise specified by the manufacturer, repairs of nicks, scratches, gouges, etc. on aluminum propeller blades must be made
- What method would be used to inspect an aluminum propeller blade when a crack is suspected
- Which of the following generally renders an aluminum alloy propeller unrepairable?
The
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Aviation Mechanic - Powerplant
test bank, click here.
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