As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DOUBLER REPAIR ACCOMPLISHED ON EXTERNAL FUSELAGE SKIN JUST AFT OF FRAME 1 & AT Y-330 RT. ORIGINAL SKIN THICKNESS 0.055INCHES. REPAIR ACCOMPLISHED IAW SRM 53-00-11 TBL 203 PARA 4 W FIG 239. REPAIR REQUIRES INSPECTION IAW SRI 53-00-11-2-017-00 PARA 3 L TBL 225. INITIAL INSPECTION AT 60000FC FROM TIME OF REPAIR EMBODIMENT.