What was found
CRACK ON BEAM AFT EDGE AND FWD EDGE AT L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02, FIG 201 AND 202, 51-40-02, 51-40-05, AND 51-10-04. PAR 15 AND 21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON BEAM AFT EDGE AND FWD EDGE AT L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02, FIG 201 AND 202, 51-40-02, 51-40-05, AND 51-10-04. PAR 15 AND 21.