What was found
INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 133 BETWEEN LONGERONS 18L AND 19L. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-10-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 133 BETWEEN LONGERONS 18L AND 19L. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-10-3.