As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND IN THE RIGHT HAND FUSELAGE SKIN AT F.S. 498.25 ABOVE STRINGER 10R. THE CRACK RADIATES THROUGH A RIVET HOLE. MAINTENANCE REPAIRED THE AFT FUSELAGE SKIN AT F.S. 498.25 AND COMPLIED WITH REQUIRED RII INSPECTIONS IAW EO 09-1900-53-027. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.