The FAA
Airline Transport 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
Airline Transport 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
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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
Airline Transport 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
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| Sample Questions
from the FAA
Airline Transport Pilot
Test Bank |
- How does high density altitude affect helicopter performance?
-
(Refer to appendix 2, figure 13.)
Given the following conditions, what is the takeoff distance over a 50 foot obstacle?
Pressure altitude 2,000 ft
Temperature (OAT) +15 °C
Weight 16,600 lb
Wind component Calm
Ice vanes Retracted
-
(Refer to appendix 2, figure 14.)
Given the following conditions, what is the accelerate-stop field length?
Pressure altitude 2,000 ft
Temperature (OAT) -15 °C
Weight 16,000 lb
Wind component 5 kts TW
Ice vanes Extended
-
(Refer to appendix 2, figures 19 and 20.)
At what altitude is the service ceiling with one engine inoperative for Operating Conditions BE-30?
-
(Refer to appendix 2, figures 27 and 28.)
What are the approach speed and ground roll when landing under Operating Conditions B-36?
-
(Refer to appendix 2, figures 27 and 28.)
What is the total runway used when touchdown is at the 1,000-foot marker for Operating Conditions B-38?
-
(Refer to appendix 2, figure 36.)
Given the following conditions, what is the maximum allowable measured gas temperature (MGT) during the power assurance check?
Engine torque 54 percent
Pressure altitude 500 ft
Temperature (OAT) +25 °C
-
(Refer to appendix 2, figure 37.)
What is the maximum gross weight for hovering in ground effect at 7,000 feet pressure altitude and +35 °C?
-
(Refer to appendix 2, figure 38.)
What is the maximum gross weight for hovering out of ground effect at 6,000 feet pressure altitude and +15 °C?
-
(Refer to appendix 2, figure 39.)
What is the takeoff distance over a 50-foot obstacle?
Pressure altitude 5,000 ft
Temperature (OAT) -10 °C
Gross weight 11,000 lb
-
(Refer to appendix 2, figure 40.)
What is the climb performance with both engines operating?
Pressure altitude 7,500 ft
Temperature (OAT) +5 °C
Heater ON
-
(Refer to appendix 2, figure 41.)
What is the single-engine climb or descent performance?
Pressure altitude 7,500 ft
Temperature (OAT) 0 °C
-
(Refer to appendix 2, figure 41.)
Given the following, what is the single-engine climb or descent performance?
Pressure altitude 1,500 ft
Temperature (OAT) +45 °C
-
(Refer to appendix 2, figure 43.)
What is the single-engine landing distance over a 50-foot obstacle?
Gross weight 14,000 lb
Pressure altitude 1,000 ft
Temperature (OAT) +10 °C
- What effect does high relative humidity have upon the maximum power output of modern aircraft engines?
-
(Refer to appendix 2, figures 27 and 28.)
What is the landing distance over a 50-foot obstacle for Operating Conditions B-36?
-
(Refer to appendix 2, figure 39.)
What is the takeoff distance over a 50-foot obstacle?
Pressure altitude 3,500 ft
Temperature (OAT) +20 °C
Gross weight 15,000 lb
- Which is a definition of V2 speed?
- (Refer to appendix 2, figure 42.) What is the airspeed limit (VNE)?
Gross weight 17,500 lb
Pressure altitude 4,000 ft
Temperature (OAT) +10 °C
- (Refer to appendix 2, figure 42.) Given the following, what is the airspeed limit (VNE)?
Gross weight 16,500 lb
Pressure altitude 5,000 ft
Temperature (OAT) -15 °C
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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