What was found
CRACK ON BEAM NR 1, FWD EDGE AT MAIN ENTRANCE DOOR. BEAM NR 1 WAS REPAIRED IAW SRM 52-10-02, FIG 201, REPAIR 7. LENGTH OF CRACK = 0.800".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON BEAM NR 1, FWD EDGE AT MAIN ENTRANCE DOOR. BEAM NR 1 WAS REPAIRED IAW SRM 52-10-02, FIG 201, REPAIR 7. LENGTH OF CRACK = 0.800".