As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INCOMING FLUORESCENT PENETRANT INSP OF HPC 1-2 SPOOL REVEALED CRACK INDICATIONS IN 2 OF DOVE TAIL POSTS ALONG THE EDGE OF BEDDING MARK. ON 1 OF POST, THE CRACKING EXTENDS ACROSS BOTH THE FWD AND AFT FACES. CRACKING MEASURED AT 1.5 INCHES AND 0.375 INCHES. THE OEM HAS BEEN INFORMED. REF MFG ACKNOWLEDGEMENT GEN M11O 09-06/ CMF56-5B, HPC 1-2 SPOOL- CRACK STG 2 DOVETAIL.