PPL(A) PL020 - General Knowledge
questionbaseoof the official questions in poland PPL(a)
questionbaseoof the official questions in poland PPL(a)
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Cartes-fiches
The element connecting and mounting the propeller on the shaft is:
The element dampening the engine vibrations transferred to the airframe is called:
The element directly opening the valves is:
The element transforming the torque is:
The sealing element between the piston and the cylinder is:
The element preserving the valves in the closed position is:
Wing elements the anti-icing installation is installed on:
Possible swarf generated during engine operation can be detected in:
Carburetor is used for:
Where can the pilot find information on the engine operating limitations:
The main parameters of the engine controlled by the pilot are:
How many colors the aircrafts navigation lights has:
How many conductors does the aircraft DC installation consist of:
How many freedom degrees has the artificial horizon:
How many freedom degrees has a turn indicator:
The oilamount in the engine is usually controlled using:
Information concerning the power of the propeller drive unit is provided by the measurement of:
The fire protection installation is mainly built:
Flight Operation Manual:
How do we call the measuring element (sensitive) of the Altimeter:
What is the value of frequency in the AC network of an aircraft:
What should be the minimum battery voltage of an airplane:
What energy is processed while charging the battery:
What energy is processed while discharging the battery:
What does the turn coordinator indicates in coordinated turn:
What air unit is used to measure the power units angular velocity
What instrument is used to measure fuel in the tanks during the flight:
What instrument determines the attitude of an aircraft during the flight:
What de-icing agent is used in anti-icing installation during the flight:
What pressure one can find on an airplane:
What action should be taken when during the pre flight inspection of the aircraft if a pilot finds pneumatic landing gear damage:
What parts of the engine are equipped with the anti-icing system:
Which major airframe parts are protected against icing:
Which instruments are designed to determine the aircraft engine state:
Which indications are showed by the DC voltmeter:
What type are icing signaling devices:
The quality of engine lubrication is controlled by measuring of :
Fuel consumption is expressed in:
Uniqueness of the bearing in the radiocompass is obtained:
Pressure Cabin:
