What was found
INSPECTION FOUND LT FUSELAGE FILLET PANEL MATING SURFACE CORRODED AT STA 756 TO 832. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-4, 51-10-3, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND LT FUSELAGE FILLET PANEL MATING SURFACE CORRODED AT STA 756 TO 832. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-4, 51-10-3, AND 51-30-2.