The EASA
ATPL Performance
test bank contains questions pertaining to
032-03-04 Climb
. 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:
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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 |
- What is the effect of tail wind on the time to climb to a given altitude?
- At MSL, in ISA conditions, climb gradient = 6 %. What would the climb gradient be if:Pressure altitude: 1000 ftTemperature: 17° CEngine anti-ice: onWing anti-ice: on(- 0.2 % engine anti-ice, - 0.1 % wing anti ice, + - 0.2 % per 1000 ft pressure altitude, + - 0.1 % per 10 ISA deviation)
- Which speed provides maximum obstacle clearance during climb?
- For an aircraft climbing at a constant IAS, the True airspeed (i) and the Mach number (ii) will :
- Compared to the gross gradient of climb the net climb gradient will be:
- A constant headwind component:
- A four jet-engine aeroplane (mass = 150 000 kg) is established on climb with all engines operating. The lift-to- drag ratio is 14. Each engine has a thrust of 75 000 Newton’ s. The gradient of climb is: (given: g= 10 m/s2):
- The best rate of climb at a constant gross mass
- The main reason for using the stepped climb technique is to:
- An aircraft has a climb speed schedule of 250 KIAS / 0.8 M. If the climb TAS is increased to 270 KIAS the Mach limit will be reached :
- The lowest point of the drag or thrust required curve of a jet aeroplane, respectively, is the point for:
- As altitude increases the stalling speed of an aircraft in terms of (i) IAS, (ii) TAS and (iii) Mach number will...
- What happens to the drag of a jet aeroplane if, during the initial climb after take off, constant IAS is maintained?(Assume a constant 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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