Lycoming TIO-540-J2BD
Service difficulty reports · 868
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'TIO540J2BD' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'TIO540J2BD' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 96ZZZX1123Magneto · defectiveMAGNETO CAME INSTALLED ON FACTORY OVERHAULED ENGINE. WHEN CONNECTING IGNITION HARNESS, NOTED RETARD LEAD COULD BE PUSHED ALL THE WAY INTO THE MAG WITHOUT TOUCHING CONTACT FINGER SPRING. REAR COVER REMOVED TO ADJUST FINGER AND RIGHT POINT SET FOUND LOOSE, ANDSDR AU960174Nut · loose(AUS) ENGINE THERMOSTATIC OIL COOLER BYPASS VALVE (VERNATHERM) NUT LOOSE - FOUND DURING INSPECTION IAW AD/LYC/78SDR CA960202011Tappet Body · surface wear(CAN)REGROUND TAPPET BODIES WERE REUSED AT OVERHAUL AND SUFFERED PREMATURE WEAR AND WORE DOWN SEVERAL CAM LOBES. ENGINE PERFORMANCE WAS DETERIORATING, ALTHOUGH NO METAL PARTICLES WERE FOUND IN THE ENGINE.SDR AU960002Bearing · failed(AUS) ENGINE NO4 CONNECTING ROD BEARING FAILED IN AREA OF RELIEF FOR CONNECTING ROD BOLT SHANKSDR 96ZZZX463Alternator · pulley backwardsALTERNATOR PULLEY INSTALLED BACKWARDS ON SHAFT. THIS WAS A NEWLY OVERHAULED UNIT RECEIVED FROM OVERHAULER.SDR CA960103007Oil Filter · collapsed(CAN)DURING INSPECTION THE ENGINE OIL FILTER WAS FOUND COLLAPSED ON ONE SIDE. THIS WAS DISCOVERED WHEN THE OUTER CASE/CAN WAS CUT OPEN FOR INSPECTION. THE FILTER WAS CODED FO3F13-1.SDR 96ZZZX364Bolt · looseBOLTS THAT SECURE TURBO MOUNT TRUSS TO ENGINE MOUNT PYLONS CONTINUALLY WORK LOOSE. NUTS CHATTER ON THREADS AND WEAR TO A POINT WHERE RE-TORQUING IS NOT POSSIBLE. MAIN PROBLEM IS STEEL BOSS ON TURBO MOUNT EATING INTO ALUMINUM MOUNT PYLON. SUBMITTER SUGGESTS SDR 96ZZZX63Crankcase · crackedA CRACK DEVELOPED 6 HOURS AFTER MAJOR OVERHAUL FROM LYCOMING. THE CRACK WAS 2.5 INCHES TO 3 INCHES LONG. SUBMITTER BELIEVES THE CRACK MUST HAVE BEEN THERE WHEN IT LEFT THE FACTORY. THIS ENGINE WAS A FACTORY REMANUFACTURE.SDR 96ZZZX665Engine · malfunctionAFTER TAKEOFF, RT ENGINE SURGED AND PILOT NOTICED A DROP IN FUEL FLOW. PILOT ELECTED TO RETURN TO BUR. PERFORMED COMPRESSION CHECK, CHECKED PROP DOME PRESSURE, CHECKED SPARK PLUGS AND MAG TIMING, CHECKED FUEL INJECTOR FLOW, AND CHECKED DENSITY CONTROLLER CONSDR 95ZZZX4014Hose Assy · brittleTHERE IS A NR 4 'AN' LOW PRESSURE HOSE ASSEMBLY WITH FIRE SLEEVE INSTALLED THAT RUNS FROM THE NR 4 90-DEGREE FITTING ON THE DIFFERENTIAL PRESSURE CONTROLLER TO THE OIL SUMP/INDUCTION HOUSING ASSEMBLY. THE END THAT ATTACHES TO THE CONTROLLER IS IN CLOSE PROXIMSDR 95ZZZX2429Cylinder · holedDURING AN APPROACH TO LANDING, PILOT REPORTED A VIBRATON IN THE LEFT ENGINE AND OIL LEAKING FROM COWLING. A PRECAUTIONARY SHUT DOWN MADE AND PILOT MADE AN UNEVENTFUL LANDING. INSPECTION REVEALED A HOLE IN NR 1 CYLINDER UNDER THE INTAKE PUSH ROD HOUSING. THESDR 95ZZZX3084Cylinder · holeDURING AN APPROACH TO LANDING, PILOT REPORTED A VIBRATION IN THE LEFT ENGINE AND OIL LEAKING FROM THE COWLING. HE PERFORMED A PRECAUTIONARY SHUT DOWN AND MADE AN UNEVENTFUL LANDING. INSPECTION REVEALED A HOLE IN NR 1 CYLINDER UNDER THE INTAKE PUSHROD HOUSINGSDR BIER 950011Bolt · misinstalledAT COMPLIANCE WITH LYC SI 1384, FOUND TOP BOLTS FOR MOUNT INSTALLED BACKWARDS AND TOP AND BOTTOM WASHERS INSTALLED ON WRONG SIDE OF BOLT ON LYCOMING OVERHAULED ENGINE. INSP TWO MATTITUCK ENGINES AND FOUND SIMILAR DISCREPENCIES.SDR 95ZZZX2048Controller · malfunctionedENGINE MANIFOLD PRESSURE FLUCTUATED 4 INCHES IN-FLIGHT. TROUBLESHOOTING FOUND NO OBVIOUS DISCREPANCIES WITH ENGINE. DIFFERENTIAL CONTROLLER WAS CHANGED AND SYMPTOMS CURED. TEST FLOWN AND OPS CHECKED NORMAL.SDR 95ZZZX963Magneto · separatedPILOT RETURNED TO BASE AFTER NOTICING SMOKE FROM LEFT ENGINE SOON AFTER TAKEOFF. MAINTENANCE DISCOVERED LT MAGNETO HAD SEPARATED FROM ENGINE CAUSING OIL LEAK AND SMOKE. REASON FOR MAGNETO SEPARATION IS UNKNOWN. NEW NUTS AND LOCKWASHERS HAD BEEN USED DURING SDR 95ZZZX502Line · chafe/burnDURING FLIGHT, PILOT NOTICED SMOKE COMING FROM OUTBOARD OF RIGHT NACELLE. PILOT SHUT DOWN ENGINE AS A PRECAUTION AND RETURNED TO BASE. MAINTENANCE DISCOVERED OIL PRESSURE LINE FROM REAR CASE TO FIREWALL HAD COME IN CONTACT WITH EXHAUST WHICH BURNED A HOLE THSDR 95ZZZX590Bearing · failedBEARINGS ON THE RIGHT ENGINE TURBOCHARGER FAILED ALLOWING SHAFT TO JUMP UP AND DOWN PULLING SEAL AWAY AND ALLOWING OIL TO BE INTRODUCED TO THE HOT SIDE OF THE TURBO. REPLACED TURBOCHARGER AND INSPECTED RT ENGINE OIL FILTER FOR METAL. ENGINE OKAY.SDR 95ZZZX685Distributor Gear · teeth missingDURING RUN-UP BEFORE FLIGHT, FOUND BAD MAG CHECK ON LT ENGINE RT MAG. REMOVED MAG FOR INSPECTION AND FOUND WHITE PLASTIC DRIVE GEAR INSIDE MAGNETO WAS MISSING NUMEROUS DRIVE TEETH, THE REST OF MAGNETO APPEARS SERVICEABLE.
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