What was found
GSO - INSPECTION FOUND FUSELAGE SKIN LAP BUCKLED AND A .25 INCH CRACK IN STR 20L, STA 767 TO STA 804. THE EFFECTED SECTION OF SKIN AND STRINGER WERE REMOVED. A SKIN AND STRINGER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 13, SRM 53-10-3, FIGURE 1, AND SRM 51-30-2. (X)