What was found
INSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED AT STA 218, LONGERON 16L AND 18L. THE DENTS WERE COLD WORKED IAW SRM 53-04, FIGURE 38. DOUBLERS WERE INSTALLED IAW SRM 53-10, FIGURE 38 AND 51-10-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE EXTERNAL SKIN DENTED AT STA 218, LONGERON 16L AND 18L. THE DENTS WERE COLD WORKED IAW SRM 53-04, FIGURE 38. DOUBLERS WERE INSTALLED IAW SRM 53-10, FIGURE 38 AND 51-10-4.