What was found
HOU - INSPECTION FOUND A 5 INCH CRACK IN DOOR PAN AT UPPER FORWARD CORNER OF MAIN CABIN DOOR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 18A. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HOU - INSPECTION FOUND A 5 INCH CRACK IN DOOR PAN AT UPPER FORWARD CORNER OF MAIN CABIN DOOR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 18A. (X)