What was found
INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR INNER SKIN AROUND LIGHTENING HOLE LIP 13.5 INCHES FROM THE LOWER EDGE OF DOOR AND 4.5 INCHES FROM THE FORWARD EDGE OF DOOR. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5232-01091.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR INNER SKIN AROUND LIGHTENING HOLE LIP 13.5 INCHES FROM THE LOWER EDGE OF DOOR AND 4.5 INCHES FROM THE FORWARD EDGE OF DOOR. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5232-01091.