As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MECHANICALLY BLENDED 1 AREA OF CORROSION IN LH GEAR WELL, AFT LOWER SPAR WS 21 TO 23 AND MECHANICALLY BLENDED 1 AREA OF CORROSION IN RH GEAR WELL, AFT LOWER SPAR WS 30 TO 33. NDT VERIFIED CORROSION REMOVAL AND REMAINING THICKNESS. EVALUATED FINDINGS AND SUBMITTED FOR REPAIR DISPOSITION. TREATED AND PRIMED AREAS PER TEXTRON FIELD REPAIR FR-680-0126-11863.