What was found
LT WING OTBD FLAP VANE AFT INBD CORNER OF SKIN HAD A GOUGE PENETRATING INTO THE INTERNAL DOUBLER. A SRM 51-70-2 PAR 18B HOT BOND REPAIR WAS INSTALLED THAT EXTENDED AROUND THE VANE LEADING EDGE. THIS REPAIR WAS APPROVED BY BOEING.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING OTBD FLAP VANE AFT INBD CORNER OF SKIN HAD A GOUGE PENETRATING INTO THE INTERNAL DOUBLER. A SRM 51-70-2 PAR 18B HOT BOND REPAIR WAS INSTALLED THAT EXTENDED AROUND THE VANE LEADING EDGE. THIS REPAIR WAS APPROVED BY BOEING.