PPL(A) PL020 - General Knowledge

questionbaseoof the official questions in poland PPL(a)

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The distance measured by DME is:

The distance along a line between the inclined plane and the beacon.

Perpendicular projection on the ground of the line between Aircraft and beacon.

Distance to calculate according to formula.

Approximate distance.

sequence of cylinder firing is done to:

Uniformly distribute crankshaft loads.

Uniform engine lubrication.

Reduction in fuel consumption.

More complete combustion of mixture.

Proper sequence of ignition is done to:

Reduction of torque pulsation.

Uniform engine lubrication.

Reduction in fuel consumption.

More complete combustion of mixture.

Heating the inlet to the carburetor is aimed at:

Protection against icing.

Heating the air in the cabin.

Raising the temperature of the fuel.

Heating the oil before starting.

Low-pressure tires are:

They are broad and designed for use on soft ground.

For use only on hard surfaces.

Only light aircraft.

They are narrow and designed for use on soft ground.

High-pressure tires are:

They are narrow and designed for use on hard surfaces.

They are used for use on soft ground.

Are wide and intended only for light aircraft.

They are used to use as the soft and hard surface.

Who develops, approves and make changes in the Flight Operation User Manual:

The aircraft manufacturer develops, and the State Aviation Authority approves it.

It is developed by user of airplane and approved by Quality Service.

It is developed by user of airplane and approved by the State Aviation Authority

Aircraft manufacturer's service quality develops and approves it.

The optimum engine oil temperature is ( C):

90-100.

30-40.

50-70.

140-160.

The aircraft exterior lighting consists of:

Anti-collision lights, and landing light.

Instrument panel illumination light.

Map illumination light.

Lights in the cabin.

Panels with radio systems control and steering elements are:

In the cockpit.

The electronic bands.

In the passenger cabin.

In the special vulnerabilities.

Parameters characterising power developed by a supercharged engine are:

RPM and boost pressure

RPM and fuel pressure.

Pressure and temperature of cylinder heads.

Charging pressure and oil pressure.

Engine fuel system assessment criteria parameter is:

Fuel pressure.

Fuel consumption.

Oil Pressure.

Rotational speed.

Which sequence of cycles for the four-stroke engine is correct:

Induction Compression Power Exhaust.

Compression Suction Expansion Exhaust.

Suction Compression Power Exhaust Compression.

Suction Compression Expansion Power.

Warming up the engine with hot air during the low temperature aims at:

Facilitate the start-up:

Increase in oil viscosity.

The increase in ignition energy.

Facilitate the creation of a fuel mixture.

Eavesdropping of radiocompass signals is obtained:

For the setting of a switch on the audio selector panel.

For a special one.

By pressing the radio button.

By pressing SPU button.

The basic mode of a radiocompass is:

Function of ADF, with reading QDM on Compass.

Antenna.

Frame.

ON.

Technical Log:

Is used to confirm performed technical services for the flight and the flight of the acknowledgment by the crew of an airplane in flight and sentences after maintenance work time aircraft, airplane type, etc. Intended for technical personnel and flight.

Used for the engeneers at the maintenance of an airline.

Is used for flight crew to enter resulting failure.

It is a document to confirm execution of the technical services of a higher order.

The so called working wing covering:

Rigid, carrying the load.

Used to enhance the stability of the aircraft.

Used for aesthetic purposes.

Only used on low speed aircrafts.

The so called not working wing covering:

Flexible not carrying the loads.

As part of a design to reduce the weight of the aircraft and transfer loads.

Assemblies the wings as facilitation of the construction and technology.

Used in high speed aircraft.

Auxiliary fuel feeding pumps are usually driven:

Electrically.

From the engine.

By hand.

Ejector.

The oil pump is driven:

From the engine.

Electrically.

Ejector.

Hydraulically.

The injection pump is designed to:

The fuel injection into the cylinders or the intake system.

Mixing fuel with air.

Preparation of the fuel mixture.

Injecting fuel to the carburetor.

The oil level "between the lines" on the bayonet dipstick means:

The correct amount of oil.

Abnormal amount of oil.

It should be added till the upper mark.

The one has to lower the oil level to the lower mark.

"SBY" mode in the transponder is used to:

Preparation of the transponder to work.

activation of the working transponder.

make up the flight.

Identification.

GPS receiver operation is based on:

Selecting an appropriate number of satellites.

Selecting the leading beacons.

Using an interference phenomenon.

DC generators are electric machines which are used for energy conversion:

Mechanical into electrical.

Electrical into chemical.

Chemical into electrical.

Electrical into heat.

DC generators installed on the aircrafts are built as:

Self- excited shunt generator.

Serial.

Separately excited.

Two-stage.

The indicated airspeed is defined as:

The speed indicated by the airspeed indicator.

The horizontal ground speed.

Speed of the aircraft relative to the sea.

The angular velocity.

The true airspeed is referred to as:

Airspeed of the aircraft at cruising altitude.

the speed of an aircraft ground

angular velocity

the speed indicated by the speedometer

The Magneto test is performed:

During the preflight check, and whenever we find it necessary.

Before each takeoff.

In-flight.

During the checks after flight.

What should be swiched off before the propeller is rotated:

Magnetos.

Battery.

Alternator.

Radio.

Carburettor throttle is controlled by:

Motor control Lever.

Engine speed controller.

Propeller pitch controller.

Pressure Difference.

When a generator or alternator fails, how much battery-life remains for a safe landing:

0,5 h - 1 h.

3 h - 4 h.

5 h - 6 h.

7 h - 8 h.

IDENT button in the transponder is used:

At the request of the air traffic control.

In order to stabilize the frequency.

To switch off.

In order to improve propagation.

The reason for detonation combustion is:

Too low octane fuel or late ignition.

The high octane fuel.

Too much oil in the fuel.

Too low ignition energy.

The allocated frequency band in VHF range for radio communication in civil aviation is:

118.00 - 136.975 MHz.

105.00 - 131.00 MHz.

95.00 - 101.00 MHz.

76.00 - 98.00 MHz.

Radiocompas can work as:

Radio ranger providing information on the location of the aircraft relative to the radio beacon as medium wave radio.

Short wave radio reciever.

The device to measure distances.

Vibration indicator.

Radiocompass has:

Two antennas.

The three antenna.

Four antennas.

Has no antenna.

Radiocompass is designed to:

Navigating an aircraft with radio beacons.

To transmit alarm signals.

To carry on external communications.

For communicating between crew members.

VHF radio station is supplied by

DC.

AC 115V.

AC 36V.

AC and DC.

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