What was found
INSPECTION FOUND THE LT FUSELAGE SKIN DENTED AT STA 200-237, LONGERON 17L. THE DENTED AREA WAS CUT OUT. A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-04, FIGURE 47.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND THE LT FUSELAGE SKIN DENTED AT STA 200-237, LONGERON 17L. THE DENTED AREA WAS CUT OUT. A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-04, FIGURE 47.