As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FS 280, RIGHT WEB CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. ORIGINAL MAT THICKNESS OF WEB .040 MAX MAT. REMOVED .012 MAT REMAINING .028 WEB IS OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. R & R L WEB IAW 53-11-10-201-003-A01.