What was found
INSPECTION FOUND A .5 INCH CRACK IN STIFFENER AT LT FUSELAGE FILLET AREA, STA 579 LONGERON 24L. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN STIFFENER AT LT FUSELAGE FILLET AREA, STA 579 LONGERON 24L. A REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2.