What was found
FUSELAGE SKIN CORRODED BETWEEN FS 559+80 TO FS 559+112 AT STR 23R. REMOVED LIGHT CORROSION IAW SRM 51-21-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CORRODED BETWEEN FS 559+80 TO FS 559+112 AT STR 23R. REMOVED LIGHT CORROSION IAW SRM 51-21-06.