What was found
CRACK ON CUSP WEB BS 864-868 BETWEEN X=+54 TO X=+60. REMOVED DAMAGE AND FABRICATE A REPAIR IAW SRM 53-05, FIG 131, A-1, SH 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON CUSP WEB BS 864-868 BETWEEN X=+54 TO X=+60. REMOVED DAMAGE AND FABRICATE A REPAIR IAW SRM 53-05, FIG 131, A-1, SH 1.