As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON TAKEOFF ROLL FROM RWY 24L-ANC, A VIBRATION BEGAN & INCREASED IN INTENSITY. AT 100 KTS IT BECAME VERY SEVERE. T/O WAS REJECTED AT 110 KTS. VIBRATION SEEMED MOST SEVERE IN NOSE GEAR REGION OR MAIN GEAR. DURING DECELERATION, A/C PULLED TO THE RIGHT. PERFORMED AIRFRAME VIBRATION INSPECTION IAW BMM 05-51-38. NOSE TIRE FOUND TO BE OUT OF BALANCE. REMOVED & REPLACED RIGHT NOSE TIRE WHEEL ASSY IAW BMM 32-45-02. SPIN & AXLE CHECK GOOD.