What was found
CRACK ON CUSP WEB BS 250 RBL 58. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 215, SRM 51-41-02, AND SRM 51-10-04 PAR 15, 21, 38.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON CUSP WEB BS 250 RBL 58. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 215, SRM 51-41-02, AND SRM 51-10-04 PAR 15, 21, 38.