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The scope of work of the radio altimeter is:

0-1200m

15-1350m.

50-450m.

Above 2000m.

0-1200m

15-1350m.

50-450m.

Above 2000m.

The turn indicator, a gyroscopic device is characterized by the fact that it:

Measures the speed of precession angles.

It has the main horizontal axis.

Measures the deviation of the direction of magnetic lines of the plane of the horizon.

Measures the aerodrome pressure.

Measures the speed of precession angles.

It has the main horizontal axis.

Measures the deviation of the direction of magnetic lines of the plane of the horizon.

Measures the aerodrome pressure.

Ignition of the fuel blend in a four-stroke engine takes place between:

Compression and Expansion.

Expansion and exhaust.

Suction and compression.

The exhaust and suction.

Compression and Expansion.

Expansion and exhaust.

Suction and compression.

The exhaust and suction.

The main fuel feed pump is driven:

From the engine.

Electrically.

Ejector.

In fluid.

From the engine.

Electrically.

Ejector.

In fluid.

Hydraulic accumulator (hydroaccumulator):

It serves as an essential aid system hydraulic system with a drop in the pressure.

As an essential source of power of the hydraulic system.

As an essential source of power in hydraulic brake system.

A hydraulic amplifier in the control system.

It serves as an essential aid system hydraulic system with a drop in the pressure.

As an essential source of power of the hydraulic system.

As an essential source of power in hydraulic brake system.

A hydraulic amplifier in the control system.

Mark the altering current (AC) sources:

AC generator or inverter/

Battery.

DC generator.

DC motor.

AC generator or inverter/

Battery.

DC generator.

DC motor.

Mark the direct current (D.C.) sources:

DC generator or alternator.

Inverter.

AC generator.

AC motor.

DC generator or alternator.

Inverter.

AC generator.

AC motor.

Too little valve clearance can cause:

Erosion and valve burnout.

Breaking of valve stem.

Oil leakage from the cylinder.

It does not matter.

Erosion and valve burnout.

Breaking of valve stem.

Oil leakage from the cylinder.

It does not matter.

With the increase of the engine speed the torque:

Increases and then decreases.

Increases.

Remains unchanged.

Decreases.

Increases and then decreases.

Increases.

Remains unchanged.

Decreases.

With the increase of the compression ratio the used fuel should be:

Higher octane.

Lower octane.

Higher cetane.

The lower temperature.

Higher octane.

Lower octane.

Higher cetane.

The lower temperature.

A set of communications equipment consists of:

FM Radio Station, ASP (Audio Selector Panel from Russian SPU) and the headphones and microphones.

Radio Station HF and SGU.

Radio Station medium frequency and microphones.

Headphones and control groups.

FM Radio Station, ASP (Audio Selector Panel from Russian SPU) and the headphones and microphones.

Radio Station HF and SGU.

Radio Station medium frequency and microphones.

Headphones and control groups.

Cavitation effect influences the fuel system:

Negatively.

Positively.

It has no effect.

It depends on the quality of the fuel.

Negatively.

Positively.

It has no effect.

It depends on the quality of the fuel.

Carburettor icing phenomenon usually occurs under the conditions of high humidity and ambient temperature of (?C):

(-1) to 12.

(-1) to 4.

Below -4.

(-1) to 12.

(-1) to 4.

Below -4.

Unit fuel consumption while leaning the fuel mixture:

Decreases and then increases.

Remains unchanged.

Increases and then decreases.

Increases.

Decreases and then increases.

Remains unchanged.

Increases and then decreases.

Increases.

The distance gyromagnetic compass is designed to:

Determine the gyromagnetic heading when changing the position of the aircraft about the vertical axis.

The geographical heading.

Airspeed.

Aircraft bank.

Determine the gyromagnetic heading when changing the position of the aircraft about the vertical axis.

The geographical heading.

Airspeed.

Aircraft bank.

Fin control:

Provides longitudinal and directional stability and controllability.

Provides directional control.

Provides longitudinal controllability.

Provides longitudinal stability.

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

Provides longitudinal and directional stability and controllability.

Provides directional control.

Provides longitudinal controllability.

Provides longitudinal stability.

What is measured by the airspeed indicator:

Speed of AN aircraft against the surrounding air masses.

Pressure at the Airport.

Heading of the aircraft.

Altitude.

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

Speed of AN aircraft against the surrounding air masses.

Pressure at the Airport.

Heading of the aircraft.

Altitude.

The aircraft moves along the taxiway. Accidentally activated transmitter blocked the radio frequency. The pilot has seen the continuous red signal transmitted from the Tower in his direction. This means that:

Stop immediately.

Taxi out of runway in use.

Return to the apron.

Cleared to taxi with increased caution.

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

Stop immediately.

Taxi out of runway in use.

Return to the apron.

Cleared to taxi with increased caution.

The sensitive measurement element of the airspeed indicator is:

differential membrane can

Burdon Tube

aneroid can

Rubber diaphragm

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

differential membrane can

Burdon Tube

aneroid can

Rubber diaphragm

The measuring (sensitive) element of the altimeter is:

Aneroid capsule.

Rubber diaphragm.

Burdon Tube.

Differential capsule.

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

Aneroid capsule.

Rubber diaphragm.

Burdon Tube.

Differential capsule.

Braking with the use of the landing gear wheels is:

Hydraulic or pneumatic.

Pneumatic-electric.

Pneumatic

Electrical

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

Hydraulic or pneumatic.

Pneumatic-electric.

Pneumatic

Electrical

What pressures are supplied to the airspeed indicator:

Static and total.

Dynamic and static.

Dynamic and total.

Total.

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

Static and total.

Dynamic and static.

Dynamic and total.

Total.

What pressure is supplied to the altimeter:

Static.

Dynamic and static.

Total and dynamic.

Total.

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

Static.

Dynamic and static.

Total and dynamic.

Total.

What are the parameters read from the altimeter:

Altitude and pressure of the aerodrome.

Pressure of the aerodrome.

Altitude.

Height of an aerodrome.

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

Altitude and pressure of the aerodrome.

Pressure of the aerodrome.

Altitude.

Height of an aerodrome.

The semi- monocoque construction fuselage consists of:

Frames, stringers, coverage.

Beams, frames, cover.

Frames, stringers, girders.

Coverage, stringers, girders.

Tastatur-Befehle:

= drehen,

= vor-/rückwärts,

= scrollen

Frames, stringers, coverage.

Beams, frames, cover.

Frames, stringers, girders.

Coverage, stringers, girders.

The monocoque construction fuselage consists of:

The main element is cover reinforced by ribs.

Frames, extension, coverage.

Girders, decking, bulkheads.

Girders, cover, honeycomb core.

The main element is cover reinforced by ribs.

Frames, extension, coverage.

Girders, decking, bulkheads.

Girders, cover, honeycomb core.

The balance tab is used to:

Reducing the forces acting on the elements of control and ailerons controls.

Trimming of an airplane.

Facilitation flaps extension.

Increased stability of an airplane.

Reducing the forces acting on the elements of control and ailerons controls.

Trimming of an airplane.

Facilitation flaps extension.

Increased stability of an airplane.

The coulor of handles and levers in the cockpit is:

The colors of individual levers and handles are normalized, depending on the type of the lever.

The colors are arbitrary.

Colors are set by an constructor.

Levers color does not matter.

The colors of individual levers and handles are normalized, depending on the type of the lever.

The colors are arbitrary.

Colors are set by an constructor.

Levers color does not matter.

Mass balance is:

Used to eliminate self-excited vibration of aileron and rudder.

Used to eliminate vibration of flaps.

Used to eliminate vibrations of aerodynamic brake.

Used to eliminate vibration of control surfaces at low speeds.

Used to eliminate self-excited vibration of aileron and rudder.

Used to eliminate vibration of flaps.

Used to eliminate vibrations of aerodynamic brake.

Used to eliminate vibration of control surfaces at low speeds.

Ailerons are used to:

Controling bank around longitudinal axis.

Maintaining the stability of the aircraft.

Longitudinal controllability.

Directional controllability.

Controling bank around longitudinal axis.

Maintaining the stability of the aircraft.

Longitudinal controllability.

Directional controllability.

PPL(A) PL020 - General Knowledge

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