As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON SUPPORT ANGLE AT MAIN EBAY BS380 S-23L. REMOVED CORROSION IN AN AREA OF 1' X 1' IAW SRM 51-10-02-0G-0. UT INSPECTED BLENDED AREA IAW NDTM PART 4 51-00-00 PROCEDURE 2, REMAINING THICKNESS IS 0.035'. EVALUATED CORROSION ON SUPPORT ANGLE, FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02-0G-0. REMOVED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW SUPPORT ANGLE IAW SRM 51-40-05-0G-0 AND DWG 143A7902. INSTALLED SUPPORT ANGLE PER SRM 51-40-02-0G-0 AND DWG 143A7902.