As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TAIL ENGINE INTAKE DUCT LEADING EDGE FOUND MULTIPLE CRACKS. #2 ENGINE NOSE COWL REMOVED AND REPLACED AS PER AMM 54-22-01-04, CARRIED OUT NOSE COWL ANTI-ICE SYSTEM FUNCTIONAL TEST AS PER AMM 30-22-00-700-804, FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. COMPLIED EA NO. 1-5451-T0385073P1 TITLE: PYLON STRUCTURE - TAIL PYLON/STRUT - NO 2 ENGINE INLET LEDIING EDGE ASSY REWORK PER DRAWING -MPN RE-IDENTIFICATION.