Text in force at CS29-12: from CS29-0, effective 14 Nov 2003.
Each part of the rotorcraft m ust be free from excessive vibration under each appropriate speed and power condition.
ED Decision 2003/016/RM · Source
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Text in force at CS29-12: from CS29-0, effective 14 Nov 2003.
ED Decision 2003/016/RM · Source
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