What was found
GSO - INSPECTION FOUND A .25 INCH CRACK IN FORWARD ENTRY DOOR FORWARD FRAME CUT OUT AT UPPER HINGE ARM. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, SRM 51-10-2, AND SRM 51-30-2. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
GSO - INSPECTION FOUND A .25 INCH CRACK IN FORWARD ENTRY DOOR FORWARD FRAME CUT OUT AT UPPER HINGE ARM. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, SRM 51-10-2, AND SRM 51-30-2. (X)