What was found
INSPECTION FOUND EXTERNAL FUSELAGE SKIN DENTED AT FS 230 BETWEEN LONGERON 19L AND 20L. THE DENTED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 25, 51-30-2, 51-30-4, AND 51-30-5.
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 230 BETWEEN LONGERON 19L AND 20L. THE DENTED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 25. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 25, 51-30-2, 51-30-4, AND 51-30-5.