What was found
EVIDENCE OF CORROSION FOUND ON STRINGER 20R BETWEEN BS 280 AND 295. INSTALLED STRINGER 20R FROM BS 280 TO 319 IAW SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01, REV 38.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EVIDENCE OF CORROSION FOUND ON STRINGER 20R BETWEEN BS 280 AND 295. INSTALLED STRINGER 20R FROM BS 280 TO 319 IAW SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01, REV 38.