As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK. NR 2 ENGINE LT SIDE METAL STRIP ABOVE REVERSER COWL HAS .75 INCH CRACK. NDT TO DETERMINE LENGTH OF CRACK. STOP DRILLED AND NDT TO CONFIRM CRACK. STOP DRILLED - BROKEN SHARP EDGES. TREATED, PRIMED AND FILLED STOP DRILL HOLES WITH SEALER PER EO 99-174 WITH APROVED 8110-3 DATED 11-12-99. REF: EMERY WORLDWIDE A/L. RRXA. (X)