As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND FUSELAGE FRAME ANGLE CORRODED AT STA 360 BETWEEN STRINGER 17R AND 20R. THE ANGLE WAS REMOVED IAW SRM 51-30-2. THE CORROSION WAS REMOVED IAW SRM 51-10-6. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2.