What was found
INSPECTION FOUND A 2 INCH CRACK IN UPPER CHORD ON FLOOR SUPPORT AT STA 380-400, BL 0. THE UPPER CHORD 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 UPPER CHORD ON FLOOR SUPPORT AT STA 380-400, BL 0. THE UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 51-10-02.