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 FWD AT BS 1183 BETWEEN STR 29R-28R. CUT OUT DAMAGED STR DIM 8.75 FABRICATED NEW STR FROM BAC 1498-147 7075 T62 DIM 8.875", SPLICE FROM BAC 1498-131 7075 T62 DIM 10.0625". INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.