What was found
INSPECTION FOUND A .5 INCH CRACK IN NR 8 BEAM OF MAIN CABIN DOOR. A REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 31, SHEET 9. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN NR 8 BEAM OF MAIN CABIN DOOR. A REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 31, SHEET 9. (M)