Describe types of static stability related to aircraft.

Description should include the following:

Static stability is the initial tendency or direction of movement back to equilibrium. In aviation, it refers to the aircraft’s initial response when disturbed from a given pitch, yaw, or bank.
Positive static stability is the initial tendency of the aircraft to return to the original state of equilibrium after being disturbed.
Neutral static stability is the initial tendency of the aircraft to remain in a new condition after its equilibrium has been disturbed.
Negative static stability is the initial tendency of the aircraft to continue away from the original state of equilibrium after being disturbed.

PLT480

Process/Skill Questions: