| 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.
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That said, while the following questions are intended
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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
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| Sample Questions
from the FAA
Airline Transport Pilot
Test Bank |
- How is helicopter climb performance most adversely affected?
-
(Refer to appendix 2, figure 13.)
Given the following conditions, what is the takeoff ground roll and V1 speed?
Pressure altitude 3,000 ft
Temperature (OAT) -10 �C
Weight 15,000 lb
Wind component 8 kts TW
Ice vanes Extended
-
(Refer to appendix 2, figure 14.)
Given the following conditions, what is the accelerate-stop field length?
Pressure altitude 8,000 ft
Temperature (OAT) -5 �C
Weight 14,000 lb
Wind component 4 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-26?
-
(Refer to appendix 2, figures 27 and 28.)
What is the remaining runway length when stopped after landing over a 50-foot obstacle for Operating Conditions B-37?
-
(Refer to appendix 2, figures 27 and 28.)
What is the remaining runway length when stopped after landing over a 50-foot obstacle for Operating Conditions B-39?
-
(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 43 percent
Pressure altitude 9,000 ft
Temperature (OAT) -15 �C
-
(Refer to appendix 2, figure 37.)
What is the maximum gross weight for hovering in ground effect at 4,500 feet pressure altitude and +20 �C?
-
(Refer to appendix 2, figure 38.)
What is the maximum gross weight for hovering out of ground effect at 7,000 feet pressure altitude and +35 �C?
-
(Refer to appendix 2, figure 39.)
What is the takeoff distance over a 50-foot obstacle?
Pressure altitude 6,500 ft
Temperature (OAT) 0 �C
Gross weight 13,500 lb
-
(Refer to appendix 2, figure 40.)
What is the climb performance with both engines operating?
Pressure altitude 6,500 ft
Temperature (OAT) +25 �C
Heater OFF
-
(Refer to appendix 2, figure 41.)
Given the following, what is the single-engine climb or descent performance?
Pressure altitude 3,000 ft
Temperature (OAT) +35 �C
-
(Refer to appendix 2, figure 43.)
What is the single-engine landing distance over a 50-foot obstacle?
Gross weight 12,000 lb
Pressure altitude 3,500 ft
Temperature (OAT) +30 �C
-
(Refer to appendix 2, figure 43.)
What is the single-engine landing distance over a 50-foot obstacle?
Gross weight 17,000 lb
Pressure altitude 4,000 ft
Temperature (OAT) +40 �C
-
(Refer to appendix 2, figures 27 and 28.)
What is the landing distance over a 50-foot obstacle for Operating Conditions B-40?
-
(Refer to appendix 2, figure 43.)
What is the single-engine landing distance over a 50-foot obstacle?
Gross weight 12,000 lb
Pressure altitude 3,500 ft
Temperature (OAT) +30 �C
- What is the correct symbol for minimum unstick speed?
- (Refer to appendix 2, figure 42.) What is the airspeed limit (VNE)?
Gross weight 15,000 lb
Pressure altitude 6,000 ft
Temperature (OAT) 0 �C
-
(Refer to appendix 2, figures 19 and 20.)
Which statement is true regarding performance with one engine inoperative for Operating Conditions BE-27?
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Airline Transport Pilot
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