As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT OVERWING REFUEL HOLE LANDING HAS MINOR CORROSION ON COMPLETE LANDING, 8.32 TOTAL SQ INCHES. CORROSION WAS REMOVED IAW SRM 51-74-00 & FLAP PEENED PRECAUTIONARY IAW SR M51-29-11. WITHIN SRM 57-21-11 PAGE 244 PARA 5FD LIMIT OF .020, MAX MATERIAL LOSS WAS .015 AT FWD EDGE OF LANDING. NDT IAW NTM51 -80-00-PB1 REVEALED NO RELEVANT INDICATIONS, MEETS AERODYNAMIC FLUSHNESS LIMIT OF AMM28-11-43.