The EASA
ATPL Performance
test bank contains questions pertaining to
032-02-03 Elements of 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
Performance
test bank.
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GroundSchool:
Performance
EASA ATPL Theory Test Prep Software
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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 |
- The most efficient angle of attack is:
- If level flight is maintained but the air density decreases then this would cause:
- The speed for maximum lift/drag ratio will result in:
- When approaching a wet runway, with the risk of hydroplaning, what technique should the pilot adapt?
- Climbing to cruise altitude with a headwind will:
- Landing on a runway with 5mm wet snow will:
- The induced drag of an aeroplane:
- An aeroplane is in a power off glide at best gliding speed. If the pilot increases pitch attitude the glide distance:
- Which of the following combinations adversely affects take-off and initial climb performance?
- An aircraft is climbing at VX. If the speed is increased, maintaining the power setting,
- Which of the following statements is true regarding the performance of an aeroplane in level flight?
- Increased ambient temperature allows:
- The optimum altitude
- Calculate the still air gradient of climb, given that the aircraft climbs at 1500fpm with a TAS of 300kts and there is a tailwind of 50kts.
- The speed that will attain the greatest rate of climb is where the greatest excess of:
- If mass increases, the power required curve of an aeroplane:
- What happens to VX and VY as altitude increases?
- (CAP 698 figure 3.9)Find the maximum planned landing weight to comply with the regulations, for the following conditions:Pressure altitude: sea levelTemperature: 30° CForecast wind component: 10kt headRunway length: 3000ft (hard, dry and level)
- The pilot of a light twin engine aircraft has calculated a 4 000 m service ceiling, based on the forecast general conditions for the flight and a take-off mass of 3 250 kg. If the take-off mass is 3 000 kg, the service ceiling will be:
- The minimum total drag of an aircraft in level flight occurs:
- A FLAT RATED jet engine will give:
- Which of the following factors will lead to an increase of ground distance during a glide, while maintaining the appropriate minimum glide angle speed?
- If the runway is wet, the landing distance required for a dry runway:
- If the net gradient of climb after take-off with all engines operating is 14 percent in the prevailing conditions, the horizontal distance required to reach a height of 1500ft from the screen, if the cloud base is 2000ft, would be:
- For a turboprop powered aeroplane, a 2200 m long runway at the destination aerodrome is expected to be " wet" . The " dry runway" landing distance, should not exceed:
- For an aircraft flying in conditions that would give the balked landing climb limit gradient of 2.5 percent, the rate of climb that would be achieved at a TAS of 90kts would be:
- What is the effect of runway slope on take-off performance?
- What is the effect of increased mass on the maximum rate of climb speed (all other factors considered unchanged)?
- The speed instability region is:
- Which of the following statements is true with respect to the take-off flight path (multi engine class B)?
- Considering a turbine powered aircraft, when passing 35 feet at the end of the take-off distance, the speed should not be less than
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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