The FAA
Commercial Pilot
test bank contains questions pertaining to
Aerodynamics
. 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
Commercial Pilot
test bank.
Did you know? Despite their claims of completeness,
the FAA test banks provided by several other online test preparation sources
are woefully incomplete. Read more about the
situation here. Our GroundSchool FAA written test preparation software generally
contains a much more up to date and complete question set and in no way suffers
from such deficiencies. In fact, it's the best way to prepare for your FAA written
test, period.
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
Commercial Pilot
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
study fast and efficient.
Sample Questions
from the FAA
Commercial Pilot
Test Bank |
- Lift on a wing is most properly defined as the
- Which statement is true relative to changing angle of attack?
- That portion of the glider's total drag created by the production of lift is called
- If the airspeed of a glider is increased from 45 MPH to 90 MPH, the parasite drag will be
- If the angle of attack is increased beyond the critical angle of attack, the wing will no longer produce sufficient lift to support the weight of the glider
- The best L/D ratio of a glider is a value that
- As altitude increases, the VNE of a helicopter will
- Regarding the effect of loading on glider performance, a heavily loaded glider would
- The lifting forces which act on a hot air balloon are primarily the result of the interior air
- If an airship in flight is either light or heavy, the unbalanced condition must be overcome
- Cyclic control pressure is applied during flight that results in a maximum decrease in pitch angle of the rotor blades at the "12 o'clock" position. Which way will the rotor disc tilt?
- In theory, if the angle of attack and other factors remain constant and the airspeed is doubled, the lift produced at the higher speed will be
- An airplane leaving ground effect will
- Which is true regarding the forces acting on an aircraft in a steady-state descent? The sum of all
- To produce the same lift while in ground effect as when out of ground effect, the airplane requires
- Longitudinal dynamic instability in an airplane can be identified by
- What changes in airplane longitudinal control must be made to maintain altitude while the airspeed is being decreased?
-
(Refer to figure 3.)
The L/D ratio at a 2° angle of attack is approximately the same as the L/D ratio for a
- Recovery from a stall in any airplane becomes more difficult when its
- The forward speed of a rotorcraft is restricted primarily by
- By changing the angle of attack of a wing, the pilot can control the airplane's
- The lift differential that exists between the advancing blade and the retreating blade is known as
- Can the tail rotor produce thrust to the left?
- Stall speed is affected by
- In a rapid recovery from a dive, the effects of load factor would cause the stall speed to
- If an aircraft with a gross weight of 2,000 pounds was subjected to a 60° constant-altitude bank, the total load would be
- One of the main functions of flaps during the approach and landing is to
- The maximum airspeed at which abrupt and full deflection of the controls would not cause structural damage to a glider is called the
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. |
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