What was found
ON TAKEOFF ROLL AT APPROXIMATELY 135K - SEVERE VIBRATION FELT AND SUSPECT BLOWN TIRE, NORMAL LANDING ACCOMPLISHED. ON POST-FLIGHT INSPECTION FOUND NR 8 TIRE BLOWN. REMOVED AND REPLACED NR 8 AND NR 7 WHEEL AND TIRE ASSY IAW A300 AMM CHAPTER 12-37-32. PERFORMED INSPECTION OF THE AIRCRAFT IAW A300 AMM CHAPTER 05-51-15, NO DEFECTS NOTED. PERFORMED A FUNCTIONAL TEST OF THE ANTISKID SYSTEM IAW A300 AMM CHAPTER 32-42-00, CHECK GOOD.