What was found
INSPECTION FOUND A 2 INCH CRACK IN MAIN CABIN FLOOR SHEAR WEB ANGLE AT STA 384, BL 0. THE SHEAR WEB ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN MAIN CABIN FLOOR SHEAR WEB ANGLE AT STA 384, BL 0. THE SHEAR WEB ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.