What was found
FUSELAGE FRAME BS 310 CORRODED ON THE FWD AND AFT SIDES BETWEEN S26L AND 26R. REMOVED CORRODED FRAME IAW SRM 51-42-06, 51-42-21. LOCATED, DRILLED AND INSTALLED NEW FRAME SEGMENT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME BS 310 CORRODED ON THE FWD AND AFT SIDES BETWEEN S26L AND 26R. REMOVED CORRODED FRAME IAW SRM 51-42-06, 51-42-21. LOCATED, DRILLED AND INSTALLED NEW FRAME SEGMENT.