What was found
AT C-CHECK, CRACK IN UPPER FLANGE OF RIB 13, R/W. STOP DRILL CRACK, HFEC, INSTALLED RIB REPAIR PER SRM 57-10-5. REPAIR 16 X 2 X 1. N/R 2257.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, CRACK IN UPPER FLANGE OF RIB 13, R/W. STOP DRILL CRACK, HFEC, INSTALLED RIB REPAIR PER SRM 57-10-5. REPAIR 16 X 2 X 1. N/R 2257.