What was found
INSPECTION FOUND A .5 INCH CRACK AT LOWER FORWARD CORNER OF R-2 DOOR SKIN. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 52-00-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK AT LOWER FORWARD CORNER OF R-2 DOOR SKIN. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 52-00-3.