What was found
INSPECTION FOUND A 2 INCH CRACK IN RT INBOARD END OF FLOOR SUPPORT AT BS 760, BL 0. THE CRACKED SECTION OF FLOOR SUPPORT WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, FIGURE 1 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN RT INBOARD END OF FLOOR SUPPORT AT BS 760, BL 0. THE CRACKED SECTION OF FLOOR SUPPORT WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, FIGURE 1 AND 51-30-2.