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Stability of an aircraft can be defined only when it is in ___________(a) Pitch(b) Yaw(c) Trim(d) RollThis 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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Answer» 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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