As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BECAUSE OF NR 2 ENGINE FAILURE, GENERAL INSPECTION OF HORIZ AND VERTICAL STAB WERE DONE. LT HORIZ STAB L/E PANEL 331CL NEEDED TO BE BLENDED APPROX 3 FEET FROM I/B END. APPROX .033 MATERIAL REMAINING. REPAIRED LT LEADING EDGE HORIZ STAB PANEL 331CL PER SRM 55-10-01. JOB COMPLETE.