What was found
CRACK ON LT CUSP WEB INNER FACE AT BS 898, X=44. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, REPAIR 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON LT CUSP WEB INNER FACE AT BS 898, X=44. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, REPAIR 4.