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Instrumentation | PPL(A) Aircraft General Knowledge - EASA & UK CAA

Aircraft instrumentation practice questions for PPL(A) candidates
Question 1

The angle between the true north and the magnetic north is the:

Question 2

At the magnetic poles the dip is:

Question 3

What is the definition of magnetic dip?

Question 1

Transport wander of the directional gyro indicator will occur when:

Question 2

The apparent earth rate of the directional gyro indicator is maximum at:

Question 1

When the aircraft is in a rate one turn, to complete a 270° turn, takes:

Question 2

Which instrument indicates the angular velocity around the vertical axis?

Question 3

If the slip indicator ball is displaced left from the centre in a turn to the left, in order to coordinate the turn the pilot should:

Question 4

The standard rate of turn is:

Transmission modes: HF, VHF and SATCOM

Section titled "Transmission modes: HF, VHF and SATCOM"
Question 1

What is the primary purpose of SATCOM (Satellite Communication)?

Question 2

Which of the following statements about VHF communication is correct?

Question 3

The airband frequency range (for communication and navigation) is:

Question 4

What frequency range do aircraft communication radios operate on?

Question 5

__(1)__ is used for long-range communication over oceanic regions, because __(2)__.

Question 1

What is the cylinder head temperature measured with?

Question 1

What is the advantage of a mechanical tachometer over an electrical tachometer?

Question 1

The stall warning horn starts to indicate a certain:

Question 1

The gyroscope of the attitude indicator can freely rotate around:

Question 1

Which of the following factors can cause a gyroscope to drift?

Question 2

What instrument can be used to align the directional gyro indicator?

Question 3

What is a gyroscope?

Question 4

The error caused by the iron and steel parts of the aircraft in the magnetic compass is called:

Question 5

A freely suspended spinning gyro has a tendency to:

Question 6

Which of the following instruments use gyroscopes? 1. Magnetic compass 2. Directional gyro indicator 3. Turn and slip indicator 4. Attitude indicator

Question 7

When an aircraft, which is located at the southern hemisphere accelerates in northerly direction:

Question 8

Consider an aircraft landing in a south-east direction in the northern hemisphere, the compass will indicate:

Question 9

Turning error is greatest when turning through:

Question 10

The fundamental properties of a gyroscope are: 1. rigidity in space 2. rigidity on earth 3. precession 4. low inertia 5. pendular movement

Question 11

Apparent drift of a gyroscope is influenced by the rotation of the Earth. The apparent drift in most noticeable at (1)__, while it is minimal at (2)__.

Question 12

What is 'gyroscopic drift'?

Question 13

What component of the gyroscope maintains its orientation during motion?

Question 14

A pilot in the northern hemisphere from 90° magnetic heading wants to turn to 180°.

Question 15

The angular momentum of a gyroscope increases when:

Question 16

If the aircraft is located in the northern hemisphere and is accelerating on a westerly heading the compass will show:

Question 17

Precession is defined as:

Question 18

During a turn through north at the northern hemisphere the compass will:

Question 1

The true airspeed during a climb with constant indicated airspeed:

Question 2

In what condition will the calibrated airspeed be equal to the true airspeed?

Question 3

What are the limits of the green arc on the airspeed indicator?

Question 4

When can VNE be exceeded?

Question 5

If we correct indicated airspeed with position and instrument error we get:

Question 6

If we correct equivalent aispeed with the density error we get:

Question 7

The limits of white arc of the airspeed indicator are:

Question 8

If the static port becomes clogged during descent, the airspeed indicator will:

Question 1

Which of the following instruments uses static pressure as an input? 1. Airspeed indicator 2. Vertical speed indicator 3. Directional gyro indicator 4. Altimeter

Question 2

Both, pitot pressure and static pressure are required for...

Question 3

Which of the following formulas is correct?

Question 4

The dynamic pressure:

Question 1

Which of the following devices measures pressure? 1. Aneroid capsule 2. Bimetal 3. Bourdon tube 4. Thermistor

Question 2

The manifold pressure gauge is responsible for measuring:

Question 1

In mode A the transponder:

Question 2

What statement is correct concerning transponders?

Question 1

Capacitive fuel quantity measurement can indicate the:

Question 2

Which of the following statements is incorrect regarding fuel gauges?

Question 3

Evaluate the following statements: 1. Float type fuel gauge indicates fuel mass; 2. Float type fuel gauge indication is affected by the attitude of the aircraft.

Question 1

What is the main purpose of a fuel flow meter in an aircraft?

Question 2

Which of the following statements accurately describes how total fuel consumption can be determined?

Question 3

Which of the following are methods of measuring fuel flow? 1. Fuel flow measured by volume per unit of time. 2. Fuel flow measured by mass per unit of time.

Question 4

Which of the following best describes how a basic fuel flow meter operates?

Question 1

What is the primary function of TCAS II in an aircraft?

Question 2

What does a red warning message on the Central Warning Panel (CWP) indicate?

Question 3

What additional feature is commonly included with an important warning to ensure the crew's attention is directed to it?

Question 4

What is the primary function of the Flight Warning System in an aircraft?

Question 5

Which GPWS mode is responsible for detecting excessive terrain closure rate?

Question 6

What is the primary function of the Ground Proximity Warning System (GPWS)?

Question 7

What is the correct sequence of actions when a Master Caution or Master Warning is received?

Question 8

What is the purpose of a Master Warning light in an aircraft?

Question 9

Which of the following flight parameters does GPWS primarily use to generate warnings?

Question 10

Which of the following best describes a caution message on the Central Warning Panel (CWP)?

Question 11

Select the correct statement regarding TCAS II Resolution Advisories (RAs):

Question 12

What symbol and color does TCAS II use to represent a Traffic Advisory (TA) on the display?

Question 1

Which of the following statements is correct or incorrect? 1. On LCD displays the view angle is limited; 2. LCD displays use more energy than CRT displays.

Question 1

Which of the following correctly describes how VHF and HF are used for voice communication?

Question 2

Why do aircraft communication systems use a Push-to-Talk (PTT) mechanism?

Question 1

If the static port is clogged, during climbing the vertical speed indicator will:

Question 2

The inputs for the vertical speed indicator are the following:

Question 1

If the aircraft is flying at 4500 ft by the altimeter setting 1013 hPa, what is the pressure altitude?

Question 2

If the aircraft is flying at 6000 ft indicated altitude and the altimeter is set to standard (1013 hPa), but the QNH in this region is 1002 hPa, then the:

Question 3

If QNH is set on the altimeter it will show:

Question 4

Flying with altimeter setting of 1013 hPa is called:

Question 5

An airport is located at sea level, the QNH is 1014 hPa, and the temperature is 20 °C (27 ft/hPa). What is the QFE?

Question 6

When flying through air with a temperature colder than the standard atmosphere at that height:

Question 7

The pressure with increasing altitude in the standard atmosphere is:

Question 8

If the aerodrome elevation is 945 ft, and the QFE is 985 hPa, what is the QNH? (27 ft/hPa)

Question 9

The elevation of the aerodrome is 350 ft, and the QNH is 1005 hPa. What is the QFE? (27 ft = 1 hPa)