What was found
RW INBD MAIN FLAP HAS GROOVE WORN INTO COMPOSITE ON UPPER SURFACE AT OUTBD END REPAIRED GOUGE ON RW INBD MAIN FLAP OTBD EDGE USING A VACUUM BAG HEAT BLANKET CURE. REPAIRED PER SRM 57-53-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RW INBD MAIN FLAP HAS GROOVE WORN INTO COMPOSITE ON UPPER SURFACE AT OUTBD END REPAIRED GOUGE ON RW INBD MAIN FLAP OTBD EDGE USING A VACUUM BAG HEAT BLANKET CURE. REPAIRED PER SRM 57-53-01.