As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE TRF NR 2 STRUT HAS A CRACK ON C2 MEASURING .400 AND A CRACK ON C1 MEASURING .800. OK TO CONTINUE ON 350 CYCLE REINSPCECT INTERVAL IAW M-25-172-01664 TRIGGERING TRF MOUNT INSPECTION 7256-I-11716-E FOR LARGEST CUMULATED CRACK FINDINGS FROM 0.79 INCHES TO LESS THAN 0.98 INCHES IN LENGTH FOR AREA C ONLY.