What was found
AT D CHECK, NR 1 L/E FLAP HAS CORNER BROKEN OFF T/E OUTBD. BURNISHED EDGES, HFEC AND INSTALLED DOUBLER AND FILLER PER SRM 51-10-1 AND AVITAS ENGINEERING, 98MSI.241D-1, N/R 1921.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT D CHECK, NR 1 L/E FLAP HAS CORNER BROKEN OFF T/E OUTBD. BURNISHED EDGES, HFEC AND INSTALLED DOUBLER AND FILLER PER SRM 51-10-1 AND AVITAS ENGINEERING, 98MSI.241D-1, N/R 1921.