What was found
FUSELAGE FRAME, BS 333 IS CORRODED BETWEEN S26L AND 26R. LOCATED, DRILLED AND NEW FRAME IAW SRM 51-40-11, SRM 51-42-21 & SRM 51-42-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME, BS 333 IS CORRODED BETWEEN S26L AND 26R. LOCATED, DRILLED AND NEW FRAME IAW SRM 51-40-11, SRM 51-42-21 & SRM 51-42-06.