Text in force at CAR3R-8: from CAR3R-0, effective 15 May 1956. OCR text
All parts of the airplane shall be demonstrated to be free from flutter and excessive vibration under all speed and power conditions appropriate to the operation + MANEUVER +Cy MAX A a) i) eo —" vif - ere Nv, of the airplane up to at least the minimum value permitted for Vu in § 3.184, There shall also be no buffeting condition in any normal flight condition severe enough to interfere with the satisfactory control of the airplane or to cause excessive fatigue to the crew or result in structural damage. However, buffeting as stall warning is considered desirable and discouragement of this type of buffeting ts not intended. SUBPART C—STRENGTH REQUIREMENTS GENERAL