What was found
IN REF NRC S/N 00352, DURING STRINGER 21RH REMOVAL, CORROSION ON INTERNAL FUSELAGE SKIN WAS FOUND BTW FS 305-315 (SETTLEMENT AREA OF STRG 21R). IT WAS REPAIRED PER EA 81-2022-044 REV. IR
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
IN REF NRC S/N 00352, DURING STRINGER 21RH REMOVAL, CORROSION ON INTERNAL FUSELAGE SKIN WAS FOUND BTW FS 305-315 (SETTLEMENT AREA OF STRG 21R). IT WAS REPAIRED PER EA 81-2022-044 REV. IR