What was found
INSPECTION FOUND FUSELAGE SKIN DENTED AT FS 313, LONGERON 28R. THE DENTED AREA WAS REMOVED IAW SRM 53-20-00, FIGURE 6. DOUBLERS AND SHIM WERE FABRICATED AND INSTALLED IAW SRM 53-20-00, FIGURE 6 AND 51-21-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN DENTED AT FS 313, LONGERON 28R. THE DENTED AREA WAS REMOVED IAW SRM 53-20-00, FIGURE 6. DOUBLERS AND SHIM WERE FABRICATED AND INSTALLED IAW SRM 53-20-00, FIGURE 6 AND 51-21-01.