What was found
ENGINE REMOVED FOR LOW POWER AND 80 PERCENT N2 INDICATION. UPON TEAR DOWN AND INSPECTION, FOUND THE PT ROTOR RETENTION LOCK CUP AND NUT HAD LOOSENED WHICH RESULTED IN RETENTION THREAD DAMAGE. PART TOTAL CYCLES: 4,959.8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ENGINE REMOVED FOR LOW POWER AND 80 PERCENT N2 INDICATION. UPON TEAR DOWN AND INSPECTION, FOUND THE PT ROTOR RETENTION LOCK CUP AND NUT HAD LOOSENED WHICH RESULTED IN RETENTION THREAD DAMAGE. PART TOTAL CYCLES: 4,959.8.