The EASA
ATPL Instrumentation
test bank contains questions pertaining to
022-01-01 Air Data Instruments
. 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
Instrumentation
test bank.
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GroundSchool:
Instrumentation
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
Instrumentation
Test Bank |
- When climbing at a constant mach number below the tropopause through an inversion:
- Cruising at FL390, M.84 is found to give a TAS of 499kt. The ISA deviation at this level will be:
- What will the altimeter of an aircraft on the aerodrome indicate with QNH set on the subscale?
- Dynamic pressure is given by:
- A servo altimeter has a quoted accuracy of 1 mb at mean sea level. The accuracy in the standard atmosphere is:
- An aircraft is passing 6,500 ft in a descent when the static line becomes blocked. The altimeter then reads:
- During a climb after take-off from a contaminated runway, if the total pressure probe of the airspeed indicator is blocked, the pilot finds that indicated airspeed :
- When an altimeter is used for SSR it is always referenced to:
- Aircraft with pressurized cabin in flight:When switching to the alternate static pressure source, the pointer of the Vertical Speed Indicator:
- The airspeed indicator is calibrated to:
- As an airplane climbs higher, the true airspeed for a given indicated airspeed will:
- At a constant calibrated airspeed (CAS), the Mach number:
- The reading of a Mach indicator is independent of:
- The difference between static air temperature and total air temperature is known as:
- When descending through an isothermal level the TAS will .... (i), the CAS .... (ii) and the LSS will .... (iii):
- If the static line to the ASI becomes blocked during a climb, the ASI reading will:
- The velocity maximum operating (V.M.O.) is a speed expressed in:
- A pressure head is subject to the following errors:
- In a combined mach/airspeed indicator the purposes of the BARBER POLE is to indicate:
- The temperature at the airport is 23º C, what is the local speed of sound:
- Where a M/IAS indicator is being used:
- The machmeter employs:
- A pitot tube covered by ice which blocks the ram air inlet will affect the following instrument (s):
- An Air Data Computer (ADC):
- The Airspeed Indicator measures:
- An aircraft flies an altitude of 3500 feet from A, elevation 700 feet QNH 1015 mb to B, elevation 1120 feet QNH 992 mb. Assuming the altimeter sub-scale is not changed, the aircraft will arrive over B at a height of:
- CAS is IAS corrected for:
- The error in altimeter readings caused by the variation of the static pressure near the source is known as:
- When flying from low pressure to high pressure, the barometric error of an altimeter will cause the instrument to:
- VFE is the maximum speed:
- Select the correct statement:
- During a steady climb the pitot head becomes totally blocked by ice. As the climb continues the indications of the machmeter will:
- Within a temperature range of +50° and -20° C the VSI is accurate to within limits of:
- VLO is the maximum:
- Indicated airspeed corrected for position error is:
- The full International Standard Atmosphere (ISA) is assumed in the calibration of:
- The servo altimeter is better than a sensitive altimeter because:
- If the static vent becomes blocked during climb:
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
Instrumentation
test bank, click here.
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