ATPL - Airline Transport Pilot license - Principles of Flight Page 27

Domande Principles of Flight - ATPLPage 27

Which statement is correct for a side slip condition at constant speed and side slip angle, where the geometric dihedral of an aeroplane is increased ?	4 risposte
Rolling is the rotation of the aeroplane about the:	4 risposte
An example of differential aileron deflection during initiation of left turn is:	4 risposte
If the nose of an aeroplane yaws left, this causes:	4 risposte
Which statement about a jet transport aeroplane is correct during take-off with the cg at the forward limit and the trimmable horizontal stabiliser (THS) positioned at the maximum allowable aeroplane nose down position?	4 risposte
Which load factor determines VA?	4 risposte
The lift coefficient (CL) of an aeroplane in steady horizontal flight is 0.4. An increase in angle of attack of 1 degree will increase CL by 0.09. A vertical up gust instantly changes the angle of attack by 5 degrees. The load factor will be:	4 risposte
Which of the following statements is true?	4 risposte
If you increase the propeller pitch during a glide with idle-power at constant IAS the lift to drag ratio will	4 risposte
The correct drag formula is:	4 risposte

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