The EASA
ATPL Performance
test bank contains questions pertaining to
032-03-01 Take-off
. 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
Performance
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
EASA ATPL
Written Test Prep Software and Apps. Not only is it more complete and up-to-date, but is also considerably faster and more efficient as a study tool.
| Sample Questions
from the EASA ATPL
Performance
Test Bank |
- What effect, if any, does high humidity have on aircraft performance?
- If not VMBE or Vmcg limited, what would V1 be limited by:
- The effect on a too late rotation will be an:
- Can take-off be scheduled if V1
- (Refer to CAP 698 Figure 4.4)Find the field length limited take-off mass given the following data:Pressure altitude: 2500 ftTake off flap: 5° Temperature: 30° CAir conditioning: OffBalanced field length available: 6000 ftPMC: OnReported wind component: 25 kt headwindRunway slope: level
- Assuming identical runway slope and wind component values, which of the following combinations will give the most limiting take-off mass?
- With a decreased flap setting from 20° to 10° on take off the effect will be:
- If a V1 in excess of the calculated value is used for take-off then:
- Which of the following will not cause the climb limited take-off weight to decrease:
- Other factors remaining constant and not limiting, how does increasing pressure altitude affect allowable take-off mass?
- If the balanced field length required for a given weight is less than the balanced field length available :
- The time delay included in take-off calculations for the recognition and reaction to an engine failure during the take-off run is:
- Which of the following is true with regard to VMCA (air minimum control speed)?
- What is the effect of a negative runway slope?
- Regarding the obstacle limited take-off mass, which of the following statements is correct?
- If the value of the balanced V1 is found to be lower than VMCG, which of the following is correct?
- The definition of V3 is:
- Considering the undercarriage assembly, the factors that limit aircraft performance are...
- The rolling friction drag of an aircrafts wheels during take-off:
- What procedure is likely to require V1 to be reduced?
- (Refer to figure 032_5-2)In the following figure, the curves B and A represent:
- The safety margin included in the take-off graphs for Class A aeroplane calculations with all engines operating is:
- The climb limited take-off mass can be increased by:
- During the flight preparation a pilot makes a mistake by selecting a V1 greater than that required. Which problem will occur when the engine fails at a speed immediately above the correct value of V1?
- Assuming that the acceleration is constant during the take-off, if the take-off speed is increased by 3%, the Take-off distance will increase by:
- For a class A aircraft the rotation speed VR must not be less than :
- The required Take-off Distance (TOD) and the field length limited Take-off Mass (TOM) are different for the zero flap case and take-off position flap case. What is the result of flap setting in take-off position compared to zero flap position?
- The maximum depth of wet snow that the CAA recommends does not cover any part of the runway for flying operations to continue should not exceed is:
- How does runway slope affect allowable take-off mass, assuming other factors remain constant and not limiting?
- In case of an engine failure recognized below V1:
- The maximum length of stopway is not limited by:
- It is recommended that the maximum crosswind for take-off on a contaminated surface is:
- Which statement, in relation to the climb limited take-off mass of a jet aeroplane, is correct?
- Which of the following represents the minimum for V1?
- Which statement is correct?
- The effects of a contaminated runway on the field limit mass are:
- Concerning the landing gear, which of the following factors would limit the take-off mass?
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 EASA ATPL
Performance
test bank, click here.
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