As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 5A INSPECTION, THE LT AFT FUSELAGE I SKIN WAS FOUND TO HAVE MULTIPLE PARALLEL CRACKS AT FRAME 75 NEAR STRINGER 1. MAINTENANCE REMOVED THE GAMAGE AND PERFORMED A DOUBLER REPAIR TO THE AFFECTED SKIN, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.