What was found
ENGINE REMOVED DUE TO TURBINE 1 AND 2 WHEEL CYCLES. UPON VISUAL INSPECTION ON COMPRESSOR NOTED: STEP WEAR BEYOND SERVICEABLE LIMITS ON SPUR GEAR SHAFT SPLINES. FAILED NO-GO GAUGE. INSTALLED A NEW SPUR GEAR SHAFT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ENGINE REMOVED DUE TO TURBINE 1 AND 2 WHEEL CYCLES. UPON VISUAL INSPECTION ON COMPRESSOR NOTED: STEP WEAR BEYOND SERVICEABLE LIMITS ON SPUR GEAR SHAFT SPLINES. FAILED NO-GO GAUGE. INSTALLED A NEW SPUR GEAR SHAFT.