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 WAS FOUND AT FS 451.0 ON THE RELIEF CUTOUT OF STR 10R CRACK APPROX .625" IN LENGTH. MAINTENANCE REPAIRED THE CRACK IN THE FRAME RADIUS AT F.S. 451.0 AND STRINGER 10R AND PERFORMED THE REQUIRED RII INSPECTIONS I.A.W. E.O. 09-1900-53-037. MATERIALS UTILIZED FOR THE REPAIR ARE INCLUDED IN THE ENGINEERING ORDER.