As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING TAKEOFF LIGHT VIBRATION WAS FELT AFTER AIRBORNE ECAM WARNING OF NAV ADR DISAGREE PLUS FLT CONTROLS ALTN LAW, ECAM ACTION WERE PERFORMED. IN ACCORDANCE WITH AMM 32-41-12-401 THE NOSE WHEEL RT AND LT WERE REPLACED TIRE PRESS 196 PSI. IN ACCORDANCE WITH AMM 34-12-000/400-001 THE ADR 2 WAS REPLACED AND TEST OK.