As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REMOVE 10 EACH WEAR PLATES AND EXISTING DOUBLER FROM THE RCB WALL AND INSPECT WALL BASE AND REMOVE CORROSION FOR EVALUATION. BLENDED SMOOTH 4EA AREAS ON RCB WALL FWD FACE SHEET @ STA X=+27.5, X=-8.5, X=-47.5, X=-62.5 BETWEEN Z=-16 & Z=-19 LOCATION REMAINING MATERIAL THICKNESS ARE BETWEEN MIN 0.050" THICK & MAX 0.176" THICK IAW UT THICKNESS INSPECTION AND UPON EVALUATION BLENDED AREA FOUND OUT OF MD11-SRM 53-20-53 -1A-1 ALLOWABLE DAMAGE 1 REV 71.