What was found
INSPECTION FOUND A 0.050" CRACK AT EDGE OF LIGHTENING HOLE IN C-2 DOOR INTERIOR SKIN. SECOND ROW FROM LEADING EDGE CENTER OF DOOR. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01019.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 0.050" CRACK AT EDGE OF LIGHTENING HOLE IN C-2 DOOR INTERIOR SKIN. SECOND ROW FROM LEADING EDGE CENTER OF DOOR. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5232-01019.