What was found
INSPECTION FOUND VERTICAL STIFFENERS CRACKED THROUGH (2 INCH CRACK) IN MLG W/W AT BS 664, RBL 6 AND LBL 6. THE VERTICAL STIFFENERS WERE REMOVED AND REPLACED IAW SRM 51-40-01 AND 51-10-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND VERTICAL STIFFENERS CRACKED THROUGH (2 INCH CRACK) IN MLG W/W AT BS 664, RBL 6 AND LBL 6. THE VERTICAL STIFFENERS WERE REMOVED AND REPLACED IAW SRM 51-40-01 AND 51-10-02.