What was found
FUSELAGE FRAME BS 333 CORRODED ON FWD AND AFT SIDES BETWEEN STR 26L AND STR 26R. INSTALLED NEW FRAME SEGMENT IAW SRM 51-42-06 AND 51-42-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME BS 333 CORRODED ON FWD AND AFT SIDES BETWEEN STR 26L AND STR 26R. INSTALLED NEW FRAME SEGMENT IAW SRM 51-42-06 AND 51-42-21.