As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE LEFT FUSELAGE SKIN AT FS 273.25 AT STRINGER 10L. CRACK APPROXIMATELY 3.6 INCH IN LENGTH RUNNING PARALLEL TO STRINGER 10L. ABOVE CRACK AT STRINGER 10L AT NEXT RIVET LOCATION. MAINTENANCE MANUFACTURED A FILLER AND PATCH. INSTALLED BOTH AND SEALED FILLER & PATCH. REFERENCE ENGINEERING ORDER EO-09-UE153-02.