As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND A CRACK ON THE FUSELAGE FRAME AT FS 456 BETWEEN STRINGER 4L AND STRINGER 5L AT THE FORWARD LONG SNUBBER MOUNT, .75" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-007. MATERIALS UTILIZED ARE INCLUDED IN THE EO.