What was found
AT D CHECK, RT I/B SKIN FLAP DELAMINATED 54 FROM O/B END UPPER SURFACE. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8, 6 BY 4, N/R 2884.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT D CHECK, RT I/B SKIN FLAP DELAMINATED 54 FROM O/B END UPPER SURFACE. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8, 6 BY 4, N/R 2884.