What was found
AFT FUSELAGE INTERNAL FRAME BS 559+112 BETWEEN STRINGERS 26L AND 26R HAS CORROSION. REMOVED AND REPLACED THE FRAME ANGLE IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE INTERNAL FRAME BS 559+112 BETWEEN STRINGERS 26L AND 26R HAS CORROSION. REMOVED AND REPLACED THE FRAME ANGLE IAW SRM.