What was found
INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERIOR BEAM NR 2 FLANGE AFT END. REPAIRED BEAM IAW SRM 52-05, FIGURE 31, SHEET 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERIOR BEAM NR 2 FLANGE AFT END. REPAIRED BEAM IAW SRM 52-05, FIGURE 31, SHEET 3.