What was found
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 338-353 BETWEEN STRINGERS 19R AND 20R. THE DENTED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 210.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 338-353 BETWEEN STRINGERS 19R AND 20R. THE DENTED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 210.