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Home > Examination quizzes for PPL(A), PPL(H), BPL Gas, BPL Hot Air, ATPL, SPL - Sailplane, EASA Drone > Quiz ATPL - Exam test Airline Transport Pilot license > Principles of Flight

ATPL - Airline Transport Pilot license - Principles of Flight

Questions Principles of Flight - ATPL

The lift coefficient (CL) of an aeroplane in steady horizontal flight is 0.35. An increase in angle of attack of 1 degree would increase CL by 0.079. If a vertical gust instantly changes the angle of attack by 2 degrees, the load factor will be:	4 Answers
Which definition of propeller parameters is correct?	4 Answers
In twin-engine aeroplanes with right turning propellers	4 Answers
Which one of the following statements about Bernoulli's theorem is correct?	4 Answers
The unit of density is:	4 Answers
The angle of attack of a wing profile is defined as the angle between:	4 Answers
The terms 'q' and 'S' in the lift formula are:	4 Answers
The relationship between induced drag and the aspect ratio is:	4 Answers
The aeroplane drag in straight and level flight is lowest when the:	4 Answers
Which line represents the total drag line of an aeroplane?	4 Answers

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