As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
W/O 29493, NR N00177, ENGINE NR 1 AT FORWARD INBOARD LOWER HOIST POINT, THE FLANGE IS CRACKED AT IT'S BASE. FPI IAWM NTM 51-91-00 CRACK IS CONTAINED BY STOP DRILL. SWAB ETCHED DAMAGED AREA IAW TASK 70-24-01-110-34 PER GESPM STOP DRILL ACCEPTABLE PER EA 6-7223-82106 AND PER AMM 72-23-00-8-F REMOVED AND REPLACED HOIST BRKTS IAW GE MM 72-23-01