As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND SEVERAL AREAS OF CORROSION ON THE UPPER & LOWER SIDES OF PANELS 351AC & 52AC, JUST INBD OF HORIZONTAL STABILIZER REAR SPARS. BLENDED & REMOVED CORROSION IN AFFECTED AREAS, NDT FINDINGS SHOW REMAINING THICKNESS TO BE BEYOND ALLOWABLE LIMITS IAW SRM 51-10-01. DAMAGES WERE SUBMITTED FOR EVALUATION. COMPLIED WITH REPAIR S-680-0034 03RD REV DATED 6 23 15.