As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENG SUPPORT RING FOUND CRACKED AT 11-12 O-CLOCK POSITION. CLOSED PER ERA 580224-14 SECTION 3 STEP 4. DAMAGE ALLOWED PER AMM 72-54-00-210-002-A INSPECTION OF THE TURBINE CASE, STEP 4A. REVISE LOGPAGE 5501542 TO REMOVE THE PARTS REPLACEMENT REQUIREMENT WITHIN 20 FLIGHT CYCLES AND SET THE REP INTERVAL TO 500 FLIGHT HOURS.