What was found
CRACK ON LT CUSP WEB BS 665, BETWEEN X=44 AND X=56 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 226, 51-41-02, 51-10-4 PAR 15, 21 AND 37.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON LT CUSP WEB BS 665, BETWEEN X=44 AND X=56 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 226, 51-41-02, 51-10-4 PAR 15, 21 AND 37.