As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) COMPRESSOR COVER CRACKED IN AREA OF APERTURE AND PIECE BROKE AWAY. CENTRIFUGAL COMPRESSOR SCRAPPED DUE TO FOD. CRACK OCCURRED IN EXACT LOCATION AND SIZE AS INDICATED IN THE TURBOMECA ARRIEL 1 MAINTENANCE MANUAL, CHAPTER 72-30-10, FIGURE 605.