What was found
FUSELAGE SKIN CORRODED AT BS 259.5+11.5, STR 22R. REMOVED AND REPLACED SKIN SECTION PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CORRODED AT BS 259.5+11.5, STR 22R. REMOVED AND REPLACED SKIN SECTION PER SRM.