What was found
INSPECTION FOUND A CREASE IN FUSELAGE SKIN AT STA 218 BETWEEN STRINGER 16R AND 17R. THE CREASED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED IAW SRM 51-10-04 AND 53-04, FIGURE 38.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A CREASE IN FUSELAGE SKIN AT STA 218 BETWEEN STRINGER 16R AND 17R. THE CREASED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A DOUBLER WAS INSTALLED IAW SRM 51-10-04 AND 53-04, FIGURE 38.