As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE PANEL 193CR HAS FIBER GLASS EROSION ON BOTH SIDES AND DELAMINATION ON INTERIOR SIDE. ; / [01] REPAIRED EROSION DAMAGE PER SRM 53-40-70-2R-1.; [02] REPAIRED EROSION AND DELAMINATION DAMAGE PER SRM 53-40-70-2R-.; [03] MISSING REFERENCE