As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN CRACKED AT BS 275 STRINGER 15L. TRIMMED OUT THE CRACK MAINTAINING A .5 INCH MINIMUM RADIUS. HFEC INSPECTED CUT OUT. FABRICATED REPAIR PLATE FROM 2024T3 CLAD. FINISHED ALL BARE ALUMINUM WITH ALODINE AND PRIMER. INSTALLED THE REPAIR PLATE WITH THE FASTENERS. MAKING THE FRAYING SURFACES SEAL. REPAIR COMPLETED. AIRCRAFT RETURNED TO SERVICE.