As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXISTING REPAIR ON FUSELAGE SKIN BETWEEN FRAME 59 & FRAME 59A, STRINGER 38RT & STRINGER 41RT, FOUND DAMAGE ON THE EDGE OF DOUBLER. REMOVED THE EXISTING REPAIR PER SRM51-40-21. MADE THE REPAIR PARTS PER SRM 53-17-12 FIG201. INSTALLED THE REPAIR PARTS PER SRM53-17-12 FIG201.