As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE SCHEDULED MX TWO CRACKS ON TOP OF FUSELAGE AT FS 150.6 WERE DISCOVERED. TOP CENTERLINE 1 RIVET HEAD SHEARED INBD OF CRACK 1.250 INCHES LONG AND A .250 INCH CRACK LT OF CENTERLINE. MX REPAIRED AFFECTED AREA IAW EO 09-1900-53-009. REPAIR AREA APPROX 7.750 INCHES BY 4 INCHES. RII INSP COMPLIED IAW EO INSTRUCTIONS.