As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE FUSELAGE SKIN HAS A BULGE AT BS 1118 ALONG STR 27L. REMOVED DAMAGED AREA DIM 4.9" X 1.250" FABRICATED DOUBLER FROM 2024 T3 .063" DIM 14.375" X 7.375" FILLER FROM 2024 T3 .050" DIM 4.9" X 1.250". INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.