As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE SCHEDULED MX A CRACK IN THE FRAME AT THE STR CUTOUT OF STR 10 R WAS FOUND AT FS 456.0 CRACK APPROX .563" IN LENGTH. MAINTENANCE REPAIRED THE STRINGER SPLICE AT F.S. 451.0 STRINGER 10R AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1900-53-039. MATERIALS UTILIZED FOR THE REPAIR ARE INCLUDED IN THE ENGINEERING ORDER.