What was found
INSPECTION FOUND, A 1.25 INCH CRACK IN NR 1 BEAM, A .75 INCH CRACK IN NR 2 BEAM, AND A .5 INCH CRACK IN NR 3 BEAM OF MAIN CABIN DOOR. REPAIR DOUBLERS WERE 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 1.25 INCH CRACK IN NR 1 BEAM, A .75 INCH CRACK IN NR 2 BEAM, AND A .5 INCH CRACK IN NR 3 BEAM OF MAIN CABIN DOOR. REPAIR DOUBLERS WERE INSTALLED IAW SRM 52-05, FIGURE 31.