What was found
CRACK ON FLOOR PANEL IS BS 168, X -25. DAMAGE AREA WAS REMOVED, REPAIR PARTS WERE FABRICATED AND TREATED, PAINTED AND INSTALLED IAW SRM 51-70-4, FIG 2 AND 51-10-3, PAGE 14 / 21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON FLOOR PANEL IS BS 168, X -25. DAMAGE AREA WAS REMOVED, REPAIR PARTS WERE FABRICATED AND TREATED, PAINTED AND INSTALLED IAW SRM 51-70-4, FIG 2 AND 51-10-3, PAGE 14 / 21.