What was found
CRACKED UPPER AREA OF AFT VENTRAL DOOR FRAME. THE DOOR FRAME WAS REPAIRED IAW SRM 51-41-02 PAR. 7.C. (1), 51-41-05 PAR 10 FIG. 19, AND SRM 53-00-00 REPAIR 1, FIGURE 201, 51-41-02 AND 51-41-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED UPPER AREA OF AFT VENTRAL DOOR FRAME. THE DOOR FRAME WAS REPAIRED IAW SRM 51-41-02 PAR. 7.C. (1), 51-41-05 PAR 10 FIG. 19, AND SRM 53-00-00 REPAIR 1, FIGURE 201, 51-41-02 AND 51-41-05.