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 IS DENTED AT BS 1043 BETWEEN STR 21L-22L. REMOVED DAMAGE DIM .750" FABRICATED DOUBLER FROM 2024 T 3 .063" DIM 4.5" AND FILLER FROM SAME DIM .750". INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.