What was found
C/W REMOVAL OF ALTERNATOR FOR 500-HOUR INSPECTION. UPON DISASSEMBLY, ROTOR SHAFT SHEARED OFF IN AREA OF NUT (PULLEY RETAINING) THREADS. EVIDENCE OF CRACK BEING VERY OLD EXISTS. MATERIAL CORRODED IN AREA OF CRACK (SHEAR AREA).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C/W REMOVAL OF ALTERNATOR FOR 500-HOUR INSPECTION. UPON DISASSEMBLY, ROTOR SHAFT SHEARED OFF IN AREA OF NUT (PULLEY RETAINING) THREADS. EVIDENCE OF CRACK BEING VERY OLD EXISTS. MATERIAL CORRODED IN AREA OF CRACK (SHEAR AREA).