What was found
AT D CHECK, FUSELAGE FILLET PANEL 3618 CRACKED AND DELAMINATED. INSTALLED OVERLAY REPAIR PER SRM 51-40-8, 4 BY 6, N/R 3636.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT D CHECK, FUSELAGE FILLET PANEL 3618 CRACKED AND DELAMINATED. INSTALLED OVERLAY REPAIR PER SRM 51-40-8, 4 BY 6, N/R 3636.