What was found
INSPECTION FOUND A .5 INCH CRACK AT UPPER RADIUS OF MAIN CABIN DOOR PAN UPPER HINGE CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 33.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK AT UPPER RADIUS OF MAIN CABIN DOOR PAN UPPER HINGE CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 33.