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Stability of an aircraft can be defined only when it is in ___________

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Stability of an aircraft can be defined only when it is in ___________

(a) Pitch

(b) Yaw

(c) Trim

(d) Roll

This question was posed to me in an interview.

I'd like to ask this question from Aircraft Systems and Aviation in division Aircraft Systems and Aviation Overview of Aircraft Maintenance

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Right option is (c) Trim

The explanation: The stability of an aircraft can be defined only when it is in trim position. Trim position can be controlled by the pilot and is an important flight control parameter.

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