What was found
INSPECTION FOUND A .040" CRACK AT EDGE OF LIGHTENING HOLE IN C-1 DOOR INTERIOR SKIN. SECOND ROW AFT OF LEADING EDGE, CENTER OF DOOR INTERIOR. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01018.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .040" CRACK AT EDGE OF LIGHTENING HOLE IN C-1 DOOR INTERIOR SKIN. SECOND ROW AFT OF LEADING EDGE, CENTER OF DOOR INTERIOR. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01018.