Stability, Maneuverability & Controllability Quiz CPL

If the airplane attitude remains in a new position after the elevator control is pressed forward and released, the airplane displays
neutral longitudinal static stability.
positive longitudinal static stability.
neutral longitudinal dynamic stability.
Longitudinal dynamic instability in an airplane can be identified by
bank oscillations becoming progressively steeper.
pitch oscillations becoming progressively steeper.
Trilatitudinal roll oscillations becoming progressively steeper.
Longitudinal stability involves the motion of the airplane controlled by its
rudder.
elevator.
ailerons.
What changes in airplane longitudinal control must be made to maintain altitude while the airspeed is being decreased?
Increase the angle of attack to produce more lift than drag.
Increase the angle of attack to compensate for the decreasing lift.
Decrease the angle of attack to compensate for the increasing drag.
If the airplane attitude initially tends to return to its original position after the elevator control is pressed forward and released, the airplane displays
positive dynamic stability.
positive static stability.
neutral dynamic stability.
If the airplane is unstable around the lateral axis, which condition will occur?
The airplane will dive or climb (pitch) progressively steeper.
The airplane tends to yaw more than it should.
The airplane will turn (bank) progressively steeper.
Where is longitudinal stability measured?
About the lateral axis.
About the vertical axis.
About the longitudinal axis.
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