As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE FRAME BS 605 IS CORRODED FROM STRINGER 24L TO 23R. REMOVED CORROSION ON FRAME IAW SRM 51-21-06. FOUND TO BE OUT OF LIMITS IAW 53-00-00 2. LOCATED AND DRILLED THE FRAME SECTOR IAW SRM 51-40-11. INSTALLED THE FRAME IAW SRM 51-42-21, AND 51-42-06.