What was found
INSPECTION FOUND A 1.5 INCH CRACK AT FORWARD END AND A 1 INCH CRACK AT AFT END OF MAIN CABIN DOOR BEAM NR 1. 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 1.5 INCH CRACK AT FORWARD END AND A 1 INCH CRACK AT AFT END OF MAIN CABIN DOOR BEAM NR 1. DOUBLERS WERE INSTALLED IAW SRM 52-05, FIGURE 31.