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 THE AFT FUSELAGE FRAME AT FS 456 CRACKED AT THE FWD GAS STRUT MOUNT UPPER INBD NUT PLATE, BETWEEN STRINGER 4L AND 5L, 2 CRACKS 1" AND .2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-067. MATERIALS UTILIZED ARE INCLUDED IN THE EO. MAJOR REPAIR.