As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING HOLE L CRACK INDICATED BY NDT INSP CRACK IS ASSESSED AS A CORNER CRACK IN THE FRM AT THE INTERFACE WITH REAR ANGLE FITTING AT 1 O'CLOCK POSITION HOLE L REWORKED UNTIL NO CRACK INDICATION IAW SRM 51-40-30. FINAL HOLE DIAMETER 0.624"/15.849 AS DETAILED ON JPF. HOLE NTD AND BOLT REPLACED WITH HLT344VF16-34 IAW SRM 51-40-20. HOLE L COVERED BY EA 6-5710-162973 PART 2 FOR FURTHER INSPECTION.