| The FAA
Sport Pilot - Instructor and Examiner
test bank contains questions pertaining to
Aerodynamics and Performance
. 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
Sport Pilot - Instructor and Examiner
test bank.
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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
Sport Pilot - Instructor and Examiner
written test prep software. Not only is it more complete and more up to date,
but it also includes answers and explanation and has many features to make your
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| Sample Questions
from the FAA
Sport Pilot - Instructor and Examiner
Test Bank |
-
(Refer to figure 17.)
A positive load factor of 4 at 140 knots would cause the airplane to
- An aircraft wing is designed to produce lift resulting from
- The angle of attack of a wing directly controls the
- The three axes of an aircraft intersect at the
- Lift produced by an airfoil is the net force developed perpendicular to the
- At a constant velocity in airflow, a high aspect ratio wing will have (in comparison with a low aspect ratio wing)
- The resistance, or skin friction, due to the viscosity of the air as it passes along the surface of a wing is called
- The tendency of an aircraft to develop forces that further remove the aircraft from its original position, when disturbed from a condition of steady flight, is known as
- As a result of gyroscopic precession, it can be said that any
- (Refer to figure 29.) What is the approximate glide distance
Height above terrain 10,500 ft
Tailwind 20 kts
- (Refer to figure 31.) What is the total landing distance over a 50-foot obstacle
Temperature 15 C
Pressure altitude 4,000 ft
Weight 3,000 lb
Headwind 22 kts
- The objective of a cross-control stall demonstration is to
- Maximum gliding distance of an aircraft is obtained when
- The combination of lift and centrifugal force produces
- During forward cruising flight at constant airspeed and altitude, the individual rotor blades, when compared to each other, are operating at
- When is rotor downwash most prevalent in certain gyroplanes?
- Longitudinal and lateral control of a gyroplane in flight are affected by
- Which is true concerning taxi procedures in a gyroplane?
- A gyroplane will have the greatest tendency to roll during
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
Sport Pilot - Instructor and Examiner
test bank, click here.
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