What was found
INSPECTION FOUND LT EXTERIOR FUSELAGE SKIN DENTED AT STA 218, L19L. THE DENTED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 25, 51-30-2, AND 51-30-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND LT EXTERIOR FUSELAGE SKIN DENTED AT STA 218, L19L. THE DENTED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 25, 51-30-2, AND 51-30-05.