PPL(A) PL020 - General Knowledge

questionbaseoof the official questions in poland PPL(a)

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Cartes-fiches	234
Langue	English
Catégorie	Technique
Niveau	Autres
Crée / Actualisé	11.04.2022 / 30.05.2022
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What does the turn coordinator indicates in coordinated turn:

The indicator ball is in the middle position.

The ball is not in mid or max Position.

The ball is in the maximum position in the direction opposite to the A/C bank.

The ball is in the maximum position in the direction of the A/C bank.

What air unit is used to measure the power units angular velocity

Revolution counter (RPM).

Speedometer.

Fuel gauge.

Altimeter.

What instrument is used to measure fuel in the tanks during the flight:

Fuel gauge.

Tachometer.

Variometer.

Pressure gauge.

What instrument determines the attitude of an aircraft during the flight:

Artificial horizon.

Radio altimeter indicator.

Speedometer.

Tachometer.

What de-icing agent is used in anti-icing installation during the flight:

The air is collected from the engine compressor.

The exhaust gases.

Special Gas.

De-icing fluid.

What pressure one can find on an airplane:

Static and total.

Dynamic and static.

Total and dynamic.

Total.

What action should be taken when during the pre flight inspection of the aircraft if a pilot finds pneumatic landing gear damage:

Determine the degree of damage (abrasion, puncture) and report this to the maintenance and enter defects in the technical log, as a damage.

Determine the degree of wear and decide to fly or not.

Replace damaged wheel by yourself.

Report this to the maintenance without entering it into technical logbook.

What parts of the engine are equipped with the anti-icing system:

The leading edge of air intake and the carburetor of a piston engine.

Compressor blades steering.

Masking elements.

There is no such installation.

Which major airframe parts are protected against icing:

The leading edge of wings and controls.

The leading edges of the rudders and ailerons.

The leading edges of the flaps and rudders.

The leading edges of the flaps and ailerons.

Which instruments are designed to determine the aircraft engine state:

Pressure gauges, thermometers, and tachometer.

Airspeed indicator.

Altimeter.

Aviation compass.

Which indications are showed by the DC voltmeter:

Value of voltage.

Current value.

Frequency.

Value of resistance.

What type are icing signaling devices:

Mechanical and electronic.

Only electronic.

Only mechanical.

No signals.

The quality of engine lubrication is controlled by measuring of :

Temperature and oil pressure.

Temperatures of the cylinder heads.

Engine speed.

Manifold pressure.

Fuel consumption is expressed in:

g/kWh.

g/h.

g/KW.

L/h.

Uniqueness of the bearing in the radiocompass is obtained:

By using a fixed antenna and loop antenna, which gives the characteristics of the resultant cardioid pick.

By choosing the appropriate frequency.

By applying the appropriate modulation.

Pressure Cabin:

Making possibility for high altitude flights without the need for oxygen.

Prevents the ingress of water in rainfall.

Maintains constant pressure between the cabin and its surroundings.

Prevents the ingress of dust.

The semi- monocoque construction fuselage consists of the following parts:

Frames, stringers, decking.

Beams, frames, cover.

Coating, stringers, girders.

Frames, stringers, girders.

Monocoque construction fuselage consists of two parts:

Frames and coverage.

Frames, stringers, honeycomb core.

Longitudinal members, decking, girders.

Stringers, frames, cover.

When do you check the efficiency of the ignition system:

During the engine test.

After an oil change.

In-flight.

During preflight inspection.

The balance tab is used to:

The reduction of forces acting on the elements of control and ailerons controls.

Trim of an A/C

It facilitates flap deflection.

Facilitates the deflection of spoilers.

Flaps are used to:

Deflecting them, increases the lift coefficient at low speeds without increasing the aircraft, the wing angle of attack.

As an aerodynamic brakes.

To increase the lift at high speeds.

To control the roll around the latheral axis of the aircraft.

Mass Compensation:

Used to eliminate control surfaces flutter.

Used to eliminate vibration of the elevator.

Used to eliminate vibration of flaps.

Applied only to eliminate the vibrations of rudder.

Ailerons are used to:

Directional steering.

Longitudinal maneuverability.

Maintaining the stability of the aircraft.

Control aircraft around it's longitudinal axis.

Ice is removed from the wings leading edges which are secured with rubber pads (boots) with te use of:

The air under pressure.

Electrical heating elements mounted into the rubber segments.

Hot air.

The exhaust gases.

A valve control mechanism is:

Engine timing.

Driver.

Splitter.

Controller.

The power transmitted to the propeller shaft is called the ….. power:

Effective.

Necessary.

Nominal.

Indicated.

With the altitude increase, the engine power:

Decreases.

Remains the same.

Increases.

Increases and then decreases.

With the altitude increase, the altitude engine power:

It grows to the optimal altitude and then decreases.

Decreases.

Remains the same.

Increases.

Power lost to overcome the mechanical resistance with increasing oil temperature:

Decreases and then increases.

Decreases.

Increases.

Remains the same.

Ignition moment related to the angle of rotation of the engine shaft angle is called:

Ignition timing.

Delaying ignition.

Initiation of ignition.

Ignition.

What does the ignition system operation test consist of:

Measuring engine RPM drop for each system.

Determination of the maximum engine speed for each of the ignition system.

Measurement of the transit time from the engine idle RPM to maximum.

Measurement of engine vibration at takeoff power rating.

AC and DC current generators are built for the following voltage:

28 V or 12 V.

35 V.

10 V.

40 V.

A sudden lack of oil pressure indication (without an increase in oil temperature) is usually caused by:

Damaged measurement system.

Damaged battery.

Lack of oil.

Damaged oil cooler.

The lowest intensity of the Earth's magnetic field is:

The magnetic equator.

The north magnetic pole.

South magnetic pole.

Geographic pole.

The order to switch on the anti-icing installation is:

Analysis of weather forecasts for the route of flight by the crew if it forecasts icing, should be included regardless of the indications.

Activation of a icing warning system.

Should be turned on all the time during flight.

Depending on the information from air traffic services.

What is name of device that provides the necessary air cooling flow through the use of appropriately shaped fairings called:

Deflectors.

Stering.

Nozzle.

Curtains.

The presence of water in the fuel is:

Inadmissible.

Limited to the amount of about 5 ml/l.

Acceptable in the form of an emulsion.

Acceptable at high temperatures.

What does the power of electric generator mounted on the aircraft depend on:

The amount of electricity needed for the type of airplane.

The speed of the aircraft.

From the aerodrome pressure and the flight altitude.

Pressure instruments.

The GPS receiver allows to:

Recieve the current aircraft position.

The term angle of attack.

Detection of storm fronts.

Maintain communications.

Engine oil air separators due to their operation can be divided into:

Static and dynamic.

Centrifugal and dynamic.

Inertia and static.

With filter and without filter.

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PPL(A) PL020 - General Knowledge

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