As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ASD SILL ANGLE CORRODED. AFTER EVALUATION OF MIDCAP ANGLE DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED MIDCAP ANGLE IAW SRM 51-42-06-001-001-A01. DRILLED 11 PILOT HOLES IN MIDCAP ANGLE WITH NR 40 DRILL BIT IAW SRM 51-40-11-001-001-A01. DRILLED REMAINING HOLES ON SILL ANGLE INSTALLED NUTPLATES ON ANGLE REF DWG SH670-31825 AND SRM 51-45-00-001-001-A01.