As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
***CORROSION*** ON SIDE PLATE; BS 772 TO 779; LBL 22; WL 154 / EVALUATED DAMAGED CORROSION; FOUND MORE 50% MAT. LOSS MAT. ORIG. .040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. ACCOMPLISHED REMOVE AND REPLACE PART ON JOB # U259139 FUSELAGE 5038