What was found
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE INNER SKIN AT BS 989.5 BETWEEN STRINGER 24L AND STRINGER 25L, CORRODED. REMOVED AND REPLACED SKIN SECTION PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE INNER SKIN AT BS 989.5 BETWEEN STRINGER 24L AND STRINGER 25L, CORRODED. REMOVED AND REPLACED SKIN SECTION PER SRM.