As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE 1ST STAGE FAN BLADE IS MANGLED BEYOND BLENDABLE LIMITS. REMOVED AND REPLACED TWO C-1 BLADES IAW MD-80 A/C MM REV 76 REV 76 SECTION 72-33-21. COMPLIED WITH TEST 6 AND 1 PER SECTION 72-00-00 PER TIMCO ENGINE CENTER CERT T48R384Y. (M)