What was found
INSPECTION FOUND A .75 INCH CRACK AT CORNER OF LOWER FORWARD INNER PAN OF FORWARD CARGO DOOR. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .75 INCH CRACK AT CORNER OF LOWER FORWARD INNER PAN OF FORWARD CARGO DOOR. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A.