What was found
CRACK ON THE NR 1 BEAM AFT EDGE AT THE L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, PROCEDURE 7, FIG 20.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON THE NR 1 BEAM AFT EDGE AT THE L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, PROCEDURE 7, FIG 20.