| The FAA
Recreational and Private Pilot
test bank contains questions pertaining to
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
Recreational and Private Pilot
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
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written test prep software. Not only is it more complete and more up to date,
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| Sample Questions
from the FAA
Recreational and Private Pilot
Test Bank |
-
(Refer to figure 8.)
Determine the pressure altitude at an airport that is 3,563 feet MSL with an altimeter setting of 29.96.
-
(Refer to figure 36.)
Approximately what true airspeed should a pilot expect with 65 percent maximum continuous power at 9,500 feet with a temperature of 36 �F below standard?
-
(Refer to figure 37.)
What is the maximum wind velocity for a 30� crosswind if the maximum crosswind component for the airplane is 12 knots?
-
(Refer to figure 39.)
Determine the approximate landing ground roll distance.
Pressure altitude 5,000 ft
Headwind Calm
Temperature 101 �F
-
(Refer to figure 40.)
Determine the total landing distance to clear a 50-foot obstacle in a gyroplane. The outside air temperature (OAT) is 80 �F and the pressure altitude is 3,500 feet.
-
(Refer to figure 41.)
Determine the total distance required for takeoff to clear a 50-foot obstacle.
OAT Std
Pressure altitude Sea level
Takeoff weight 2,700 lb
Headwind component Calm
-
(Refer to figure 47.)
Which airspeed/altitude combination should be avoided during helicopter operations?
-
(Refer to figure 47.)
Which airspeed/altitude combination should be avoided during helicopter operations?
- Which combination of atmospheric conditions will reduce aircraft takeoff and climb performance?
-
(Refer to figure 36.)
Determine the approximate manifold pressure setting with 2,450 RPM to achieve 65 percent maximum continuous power at 6,500 feet with a temperature of 36 �F higher than standard.
-
(Refer to figure 36.)
What is the expected fuel consumption for a 1,000-nautical mile flight under the following conditions?
Pressure altitude 8,000 ft
Temperature 22 �C
Manifold pressure 20.8" Hg
Wind Calm
-
(Refer to figure 55.)
At what speed will the glider gain the most distance while descending 1,000 feet in still air?
-
(Refer to figure 58.)
What is the maximum altitude for the balloon if the gross weight is 1,000 pounds and standard temperature exists at all altitudes?
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more information about the
Recreational and Private Pilot
test bank, click here.
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