The EASA
ATPL Systems, Powerplant, and Electronics
test bank contains questions pertaining to
021-03-01 Piston Engine part 1
. 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
Systems, Powerplant, and Electronics
test bank.
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Systems, Powerplant, and Electronics
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That said, while the following questions are intended
as a general familiarization tool, this list may not be up-to-date nor accurate.
We do not update this website as often as we update our software, which will
contain at any moment all questions that we have for a given test / topic. Therefore,
if you need to actually study for your test, instead of using the list below,
we strongly, strongly encourage you to download our GroundSchool
EASA ATPL
Written Test Prep Software and Apps. Not only is it more complete and up-to-date, but is also considerably faster and more efficient as a study tool.
| Sample Questions
from the EASA ATPL
Systems, Powerplant, and Electronics
Test Bank |
- Icing of the carburettor can take place?
- As engine speed increases the ignition spark:
- In an aircraft equipped with a float-type carburettor and a constant-speed propeller, carburettor icing would probably first be detected by:
- When priming a piston engine, fuel is induced into:
- The propeller blade angle is defined as the acute angle between the airfoil section chord line (at the blade reference station) and which of the following?
- Compression ratio is the ratio between the:
- The use of a turbocharger on an engine will:
- For internal cooling, reciprocating engines are especially dependent on:
- The coolant temperature of a liquid cooled engine is controlled by:
- Swept volume is:
- Carburettor hot air is selected to:
- The action of the density controller when sensing a rise in the supercharger delivery air temperature is to:
- The presence of carburettor ice, in an airplane equipped with a fixed-pitch propeller can be verified by applying carburettor heat and noting:
- The positions of the intake and exhaust valve at the end of the power stroke are:
- An exhaust manifold leak upstream of the turbocharger will cause:
- The oil contents on a piston engine are checked:
- During the induction stroke:
- The turbo-charger waste gate is spring loaded towards:
- The kind of compressor normally used as a supercharger is:
- A turbo-supercharger impeller is driven by:
- On which stroke or strokes are both valves on a four-stroke cycle reciprocating engine cylinder open during a part of the strokes.
- In an air-cooled aero-engine, cooling air is directed around the cylinders:
- The turbocharger rpm is directly controlled by the:
- What prevents an impulse coupling operating at speeds above start speed, considering that it has flyweights?
- The very rapid magnetic field changes (flux) around the primary coil in a magneto are accomplished by the:
- What would happen if the waste gate of a turbo-charged engine seized in the descent?
- Excessive cylinder head temperatures are caused by:
- One reason for the dual ignition system on an aircraft engine is to provide for one of the following:
- When an engine starts up and the starter key is released, to what position does the key return?
- Fuel/air ratio is the ratio between the:
- Under static engine conditions, the waste gate is normally:
- If the vacuum capsule in the ABC were to be punctured in normal cruise flight, the boost pressure would:
- On modern carburettors, the variations of mixture ratios are obtained by the adjustment of:
- Static boost in a supercharged engine is:
- The strokes of a four stroke piston engine in operating order are:
- A two-stage supercharger increases the engine boost available at:
- Brake Mean Effective Pressure is:
The
list above contains 1/4 or less of the actual number of questions
and may not be up to date! Download the software today to get
access to all available questions. |
For
more information about the EASA ATPL
Systems, Powerplant, and Electronics
test bank, click here.
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