What was found
RT INBD T/E AFT FLAP WEDGE UPPER SKIN HAS CORROSION AND EXFOLIATION 44" FROM INBD END AT AFT EDGE. CUT OUT DAMAGED SKIN AND HOT BONDED A PERMANENT REPAIR DOUBLER AND FILLER IAW SRM 51-70-10-2R-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT INBD T/E AFT FLAP WEDGE UPPER SKIN HAS CORROSION AND EXFOLIATION 44" FROM INBD END AT AFT EDGE. CUT OUT DAMAGED SKIN AND HOT BONDED A PERMANENT REPAIR DOUBLER AND FILLER IAW SRM 51-70-10-2R-4.