As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ENGINE RETURNED FOR MAINTENANCE WHEN AIRCRAFT WAS EXPERIENCING ENGINE TEMPERATURE LIMIT AT TAKE OFF AND SUBSEQUENT HUNG STARTS. THE INNER HUB OF THE 4TH LOW COMPRESSOR STATOR WAS FOUND SEPARATED DURING ENGINE MAINTENANCE DISASSEMBLY. MAJOR ENGINE COMPONENT DOWNSTREAM DAMAGE OCCURED AS SECONDARY DAMAGE. ENGINE MANUFACTURER NOTIFIED OF THIS UNIQUE FINDINGS.