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Home > Training for exam quizzes ATPL, PPL(A), PPL(H), BPL Hot Air, BPL Gas, SPL - Sailplane, EASA Drone, FAA Drone > Aircraft General Knowledge - PPL(H) - Private Pilot License

Quiz Aircraft General Knowledge - PPL(H) - Private Pilot License

Test 10 Questions PPL(H) - Private Pilot License - Aircraft General Knowledge, no time limit

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1 - What does the dynamic pressure depend directly on? Lift- and drag coefficient Air pressure and air temperature Air density and airflow speed squared Air density and lift coefficient

2 - What does the slip indicator show? Airplane's bank Vertical to horizon Apparent vertical Rate of turn

3 - The bank angle of a 2-minutes circle depends on the... CAS. TAS. IAS. Ground speed.

4 - Which instrument can be affected by the hysteresis error? Direct reading compass Altimeter Vertical speed indicator Tachometer

5 - What is the reason for static dischargers on aircraft? To improve the quality of radio transmission in high altitudes To discharge static charging during flight To ensure grounding during refueling To eliminate electrical interferences during intensive radio traffic

6 - Lower-than-standard temperature may lead to... An altitude indication which is too high. A correct altitude indication as long as the altimeter subscale is set to correct for non-standard temperature. A blockage of the Pitot tube by ice, freezing the altimeter indication to its present value. An altitude indication which is too low.

7 - An aircraft in the northern hemisphere intends to turn on the shortest way from a heading of 360° to a heading of 270°. At approximately which indication of the magnetic compass should the turn be terminated? 270° 360° 300° 240°

8 - Which actions shall be taken if the engine oil pressure continuously drops to zero? Check the mixture lever and enrich the mixture Reduce engine performance and continue the flight to the destination Monitor oil temperature and land at the nearest airfield Land immediately on suitable terrain and be prepared for an autorotation

9 - A spider control... Feeds fuel by the rotational movement of pistons with various lengths. Prevents the overlay of collective and periodic control inputs on the main rotor. Changes the ignition timing of the magneto ignition during start-up. Changes the pitch angle of the rotor blades via an internal control rod.

10 - The rotor brake should be engaged (provided that no other procedure is described in the flight manual)... During all prescribed pre-flight checks on the ground. For inside parking. For outside parking. During start-up until reaching the prescribed rotor rpm.

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