What was found
INITIAL INSPECTION : CORROSION ON FLOORBEAM 27LBL BTW FS=1006 TO FS=1041 AT REAR FUSELAGE INTERNAL STRUCTURE (FUS) ( TCI:53-30-310). FLOORBEAM WAS REPAIRED PER SRM 53-00-42-201-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INITIAL INSPECTION : CORROSION ON FLOORBEAM 27LBL BTW FS=1006 TO FS=1041 AT REAR FUSELAGE INTERNAL STRUCTURE (FUS) ( TCI:53-30-310). FLOORBEAM WAS REPAIRED PER SRM 53-00-42-201-001-A01.