ATPL - Airline Transport Pilot license - Principles of Flight Page 14

Questions Principles of Flight - ATPL Page 14

During landing of a low-winged jet aeroplane, the greatest elevator up deflection is normally required when the flaps are:	4 Answers
The 'short period mode' is an:	4 Answers
The aerodynamic contribution to the static longitudinal stability of the nacelles of aft fuselage mounted engines is:	4 Answers
The effect of a ventral fin on the static stability of an aeroplane is as follows: (1=longitudinal, 2=lateral, 3=directional)	4 Answers
Static lateral stability should not be too small, because:	4 Answers
Which of the following statements concerning control is correct?	4 Answers
Examples of aerodynamic balancing of control surfaces are:	4 Answers
What should be usually done to perform a landing with the stabilizer jammed in the cruise flight position ?	4 Answers
Increase of the delta load factor due to a given vertical upgust at a given EAS occurs when:	4 Answers
Does the pitch angle of a constant speed propeller alter in medium horizontal turbulence?	4 Answers

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