As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE FUSELAGE FRAME AT FS 509.5 BETWEEN STRINGER 4L AND 5L AT THE AFT LONG SNUBBER MOUNT.1.5" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-006. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER. MAJOR REPAIR.