As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT FRAME 47 REAR SPAR HOLE 'N' SHOWS EVIDENCE OF MECHANICAL DAMAGE AT 5 O'CLOCK THROUGH THE FORWARD FITTING AND MAIN SPAR DEPTHS. MECHANICAL DAMAGE REMOVED FROM HOLE "N" IAW SRM 51-40-30 AND THE FINAL BORE DIAMETER IS 0.5605". THE MAXIMUM ALLOWED IN EO 6-5710-7-3305 PT1 IS 0.562". REWORK ACCOMPLISHED IAW EA 6-5710-162973, PAGE 8.