As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE LT MAIN GEAR WHEEL WELL DOOR INNER AFT TIRE RECESS HAS A 1 INCH GROVE AT THE FWD OTBD SIDE BLENDED AREA ORIG MAT .063 REMAINING MAT IS OUT OF LIMITS, REMOVED DAMAGE. HFEC, NO CRACKS FOUND. FABRICATED AND INSTALLED DOUBLER IAW SRM51-71-30 FIG 102.