What was found
DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BETWEEN BS 520 TO BS 530, STR 28R. REPAIRED SKIN PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BETWEEN BS 520 TO BS 530, STR 28R. REPAIRED SKIN PER SRM.