The EASA
ATPL Systems, Powerplant, and Electronics
test bank contains questions pertaining to
021-01-09 Air driven Systems (Turbo Propeller and Jet Aircraft)
. 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
Systems, Powerplant, and Electronics
test bank.
 |
GroundSchool:
Systems, Powerplant, and Electronics
EASA ATPL Theory Test Prep Software
for MS-Windows |
 | Sorry, file temporarily unavailable. Please check back soon. | |
|
|
|
|
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
Systems, Powerplant, and Electronics
Test Bank |
- In the event of failure in one of the cabin air supplies, loss of cabin pressure is prevented by:
- If the maximum operating altitude of an airplane is limited by the pressurized cabin, this limitation is due to the maximum:
- If pressurisation air supply comes from the compressor of the engine, an oil leak from the compressor bearings will:
- In the case of a thermal de-icing system over temperature, this indicated by:
- The tubes in the de-ice boots are usually inflated alternately. Why?
- The anti-ice or de-icing system which is mostly used for the wings of modern turboprop aeroplanes is:
- Assuming cabin differential pressure has reached the required value in normal flight conditions, if flight altitude and air conditioning system setting are maintained:
- With regard to the pneumatic mechanical devices which afford protection against the formation of ice, the only correct statement is:
- If pressurisation is selected before take-off the cabin rate of change indicator indicates:
- In a manually operated system, the cabin altitude rate of change is normally controlled by:
- The pneumatic system accumulator is useful:
- A typical MP pneumatic main system pressure would be:
- Water collected by the water separator may be sprayed into the ram air duct. This has the effect of:
- The vapour cycle cooler works on the principle of changing:
- The main elements of a vapour cycle cooling system are?
- If an aircraft is descending, what will happen to the cabin pressure differential?
- The rate of change of cabin pressure should be kept to the minimum. This is more important:
- The pneumatic ice protection system is mainly used for:
- State the function of a heat exchanger:
- On landing, the cabin pressure is equalized with atmospheric pressure by the operation of:
- The boots of a pneumatic de-icing system are normally made of:
- In jet aeroplanes the 'thermal anti-ice system' is primarily supplied by:
- In an aircraft air conditioning system the air cannot be treated for:
- If in cruise at 30000ft the cabin altitude is adjusted from 4000ft to 6000ft:
- The mass flow delivery from the engine driven mechanical compressors is controlled by:
- The rate of change of cabin pressure should be kept to the minimum. Is this more important:
- Safety valves operate:
- The power source for hot air in de-ice / anti ice systems on jet A/C is:
- In normal operation, the maximum cabin altitude for a large passenger aircraft is:
- A humidifier is fitted to:
- A heat exchanger functions by:
- The term " pressure differential" can be defined as the pressure difference between:
- A cabin humidifier is sometimes used:
- Typically, icing does not occur above about...
- Cabin differential pressure is the pressure difference between:
- The maximum differential pressure of a transonic transport category airplane is approximately:
- In an air cycle type air conditioning system, reduction of air temperature and pressure is achieved by:
- In a bootstrap cooling system the supply air is first:
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
Systems, Powerplant, and Electronics
test bank, click here.
Copyright,
Content, and Accuracy Notice: . Dauntless Software grants visitors
permission to use the contents of this page for personal use - commercial or
public use, including collecting (or harvesting) of any data or material on
this page is strictly prohibited. This material is presented for informational
purposes only and may be in error. Dauntless Software works hard to maintain
our EASA ATPL question banks. If you see an error on this web page, it
is likely NOT an error that is repeated in our software, as our software (unlike
this web page) is connected to our editorial mechanism whose mission is to quickly
identify and correct errors. If you see what you believe to be an error, please
download and try our software to see if the error is repeated there. If you
believe it is, you can use the issue-reporting mechanisms within the software
to contact our editors about any concern you may have and we will be happy to
look into it promptly.
<
|
