What was found
INSPECTION FOUND FORWARD FUSELAGE SKIN DENTED FIVE INCHES BELOW S17L AT STA 380 TO 400. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2 AND 53-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FORWARD FUSELAGE SKIN DENTED FIVE INCHES BELOW S17L AT STA 380 TO 400. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2 AND 53-30-3.