As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FRAME 333 HAS CORROSION SPOTS ON THE FWD AND AFT SIDES BETWEEN STRINGERS 25R AND 26L. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS .050 MATERIAL LOSS .012 REMAINING MATERIAL .038 ALLOWABLE LOSS .005 REMOVED AND REPLACED FRAME SEGMENT.