What was found
CRACK ON INNER PAN APPROXIMATELY BS 200, AFT EDGE, BETWEEN UPPER EDGE AND BEAM 1 AT MAIN ENTRANCE DOOR. INNER PAN WAS REPAIRED IAW SRM 52-10-02, REP 2, FIG 201. LENGTH OF CRACKS: 1.800", 2.400".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON INNER PAN APPROXIMATELY BS 200, AFT EDGE, BETWEEN UPPER EDGE AND BEAM 1 AT MAIN ENTRANCE DOOR. INNER PAN WAS REPAIRED IAW SRM 52-10-02, REP 2, FIG 201. LENGTH OF CRACKS: 1.800", 2.400".