As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - THE FUSELAGE FRAME AT F.S. 177 AT STRINGER 11L WAS FOUND CRACKED IN THE BEND RADIUS. CRACK LENGTH APPROX .2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-015 STEPS 1-4. MATERIALS UTILIZED ARE INCLUDED IN THE EO.