What was found
INSPECTION FOUND FUSELAGE SKIN DENTED BETWEEN LONGERON 21R AND 22R AT STA 165. THE DENT WAS COLD-FORMED AND DYE CHECKED WITH NO CRACKS FOUND. AN INTERNAL DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, PAGE 218.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN DENTED BETWEEN LONGERON 21R AND 22R AT STA 165. THE DENT WAS COLD-FORMED AND DYE CHECKED WITH NO CRACKS FOUND. AN INTERNAL DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38, PAGE 218.