What was found
INSPECTION FOUND FUSELAGE SKIN CREASED AT FS 133, LONGERON 18L. A DOUBLER AND SKIN FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 38 AND 53-34, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN CREASED AT FS 133, LONGERON 18L. A DOUBLER AND SKIN FILLER WERE INSTALLED IAW SRM 53-04, FIGURE 38 AND 53-34, FIGURE 1.