What was found
INSPECTION FOUND LT FORWARD LOWER EXTERIOR FUSELAGE SKIN DENTED AT STA 200 BETWEEN LONGERON 25L AND 26L. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 38. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND LT FORWARD LOWER EXTERIOR FUSELAGE SKIN DENTED AT STA 200 BETWEEN LONGERON 25L AND 26L. THE DENT WAS COLD WORKED IAW SRM 53-04, FIGURE 38. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-30-2.