What was found
CORROSION ON AFT SIDE OF FUSELAGE FRAME BS 333, BELOW FLOOR, BETWEEN STRINGERS 25L AND 25R. R & R SECTION OF FRAME IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON AFT SIDE OF FUSELAGE FRAME BS 333, BELOW FLOOR, BETWEEN STRINGERS 25L AND 25R. R & R SECTION OF FRAME IAW SRM.