What was found
INSPECTION FOUND A .25 INCH CRACK IN RADIUS OF MAIN CABIN DOOR NR 1 HORIZONTAL BEAM FORWARD END. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK IN RADIUS OF MAIN CABIN DOOR NR 1 HORIZONTAL BEAM FORWARD END. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31.