What was found
TAKEOFF RUN WITH V1 WAS 124 KNOTS AND ROTATION VR 136,2 KNOTS PRIOR TO ROTATION EXPERIENCED A STRONG VIBRATION AND CONTINUED WITH TAKEOFF TO ACHIEVE A SPEED OF V2 PLUS 10. ONCE AIRBORNE THE VIBRATION STOPPED. CHECKED HYDRAULICS AND FUEL QUANTITY FOR ANY, ALL SYSTEMS CHECKED FINE AND THE AIRCRAFT WAS PERFORMING AS NORMAL. COMMANDED GEAR UP AND CLIMBED TO 16,000 FEET AS A SAFE ALTITUDE.ONCE AT 16,000FT. CONTACTED THE TOWER AND ADVISED HAD A VIBRATION AND WE HAVE A POSSIBLE BLOWN TIRE,WE ASKED THAT THEY CHECK RUNWAY FOR DEBRIS.THE TOWER CONFIRMED THEY HAD A PIECE OF RUBBER POSSIBLY FROM A TIRE. AT THIS POINT THE AIRCRAFT WAS FLYING IN A CLEAN CONFIGURATION WITH NO VIBRATIONS OR ABNORMALITIES, ALL PERIMETERS WERE NORMAL.ATC ASKED WHAT MY INTENSIONS WERE, RESPONDED ALL SYSTEMS WERE NORMAL AND WERE CONTINUING TO OUR DESTINATION. DIVERTED. ON INSPECTION OF THE DAMAGE, REALIZED THE NR 2 INBOARD TIRE HAD BLOWN WHICH CAUSED SUBSEQUENT DAMAGE AND DEBRIS.