As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT 280 WEB IS CORRODED. BLENDED CORROSION ON WEB IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND IAW MAC NDT INSP PROCEDURE UT-3 MIN MATERIAL REMAINING IS .036" ORIGINAL IS .040" MATERIAL REMOVED IS .004". BLENDED AREA FOUND TO BE WITHIN LIMITS SRM 53-11-10-201-003-A01.