Lycoming TIO-540-J2B
Service difficulty reports · 63
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 = 'TIO540J2B' 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 = 'TIO540J2B' 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 JIK2008F00005Exhaust Duct · crackedAFTER DEPARTURE, AT ABOUT 1000 FEET AGL, THE PILOT REPORTED THAT THE LT ENGINE MANIFOLD PRESSURE DROPPED SUDDENLY, THE ENGINE SURGED AND THEN QUIT RUNNING. THE PILOT RETURNED TO DEPARTURE SAFELY. UPON EXAMINATION, IT WAS FOUND THAT THE EXHAUST FLANGE AT THE WSDR CA080305011Switch · intermittent(CAN) THE PILOT REPORTED THAT THE HEATER DID NOT WORK. MAINT INVESTIGATED AND DETERMINED THAT THE CYCLING SWITCH WAS DEFECTIVE AND REPLACED THE SWITCH. THE CREW AGAIN REPORTED THAT THE HEATER DID NOT WORK PROPERLY. MAINT DID MORE TROUBLESHOOTING AND DETERMINEDSDR 4022Crankshaft · failedPILOT WAS IN CRUISE, LEFT ENGINE HAD VIBRATION AND UNCOMMANDED SHUT DOWN. PILOT LANDED AT PHD. VISUAL INSPECTION REVEALED CRANKCASE DAMAGE / CRANKSHAFT HAD FAILED. REASON UNKNOWN AT THIS TIME. REPLACED ENGINE WITH NEW.SDR 2005FA0000121Bearing · failedRT REAR MAIN BEARING BEGAN TO SHRED METAL INTO OIL FILTER AFTER LANDING. OIL CHANGE AND FILTER CUT OPEN. THIS WAS FOUND ON A PRE-BUY. LETTER TO FAA SENT SEPT 03, 2005, BUT NO REPLY. (K)SDR A302004F00000Stud · shearedTHROTTLES WERE SET AT 32 OF MANIFOLD PRESS. PROPS WERE SET AT 2300 RPM. ENG GAUGES WELL IN THE GREEN. THE RT ENG MANIFOLD STARTED TO DROP. TEMPS AND OIL PRESSURE REMAINED IN THE GREEN. THE EGT STARTED TO DROP. DUE TO LOSS OF MANIFOLD PRESS, SUSPECTED A TSDR 2003FA0001135Pump · leakingFUEL LEAKING AT REGULATOR HOUSING, THIS IS THE NEW STYLE PUMP, AND IS NOT YET AFFECTED BY AD 2003-14-03. WE ARE NOTING SIMILAR LEAKS WITH SEVERAL OF THESE PUMPS.SDR 2003F00396Garlock Seal · defectiveDURING RETURN FLIGHT FROM (MYNN) INBOUND TO TMB, BETWEEN BIMINI AND MIAMI LT ENGINE OIL PRESSURE STARTED FLUCTUATING. PILOT PERFORMED PRECAUTIONARY ENGINE SHUT DOWN ON LT ENGINE. NO OTHER OCCURENCES. FINDINGS: OIL FLUCTUATING DUE TO LOSS OF OIL THROUGH HYDRAUSDR 2003FA0000761Cylinder · separatedLT ENGINE FAILED DURING CLIMBOUT AT 1500 FEET AGL, 3 MILES FROM TAKE OFF. INSPECTION REVEALED NR 2 CYLINDER SEPARATED FROM CASE, A LARGE SECTION OF THE CASE WAS BROKEN OFF AT THE NR 2 POSITION AND THE CONNECTING ROD WAS SEPARATED FROM THE CRANKSHAFT.SDR 2002FA0001388Actuator · failedNLG ACTUATOR ARM FAILED DURING GEAR EXTENSION. NOSE LANDING GEAR WOULD NOT EXTEND. AIRCRAFT LANDED. CAUSING DAMAGE TO PROP, GEAR DOORS, SKIN.SDR CA030102006Governor · malfunctioned(CAN) SLIGHT RPM HUNTING ON RT ENGINE AT CLIMB OUT POWER. PROP GOVERNORS WERE SWITCHED TO SEE IF PROBLEM WOULD MOVE. ENDED UP SENDING GOVERNOR OUT FOR REPAIR.SDR CA030102004Engine · making metal(CAN) EVENT NR 2 INSPECTION, FOUND RT ENGINE METAL PARTICLES IN OIL FILTER, BETWEEN 20-40 PARTICLES. ENGINE SERVICED WITH 15W50 OIL. AIRCRAFT GROUND RUN AND LEAK CHECKED. ONE HOUR TEST FLIGHT, OIL CHECKED AFTER FLIGHT. AT 523.6 HOURS, CUSTOMER DECIDE NOT TO FSDR CA020227003Bearing · destroyed(CAN) #6 CON ROD BEARING FAILURE. PARTS RETURNED TO SUPERIOR AIR PARTS FOR EXAMINATION.THESE BEARINGS ARE A BIMETAL AS OPPOSED TO A TRIMETAL THAT WAS USED FOR MANY YEARS. I HAVE RECIEVED REPORTS FROM AUSTRALIA OF SEVERAL FAILURES OF THIS TYPE OF BEARINGSDR CA030102003Engine · making metal(CAN) PILOT REPORTED LOW OIL PRESSURE READING 10 MINUTES PRIOR TO LANDING. VISUAL INSPECTION OF ENGINE EXTERIOR & OIL LEVEL CHECK CARRIED OUT BY PILOT. 3 LITERS OF OIL ADDED. AIRCRAFT TEST FLOWN, TAKEOFF NORMAL, RUN UP WAS NORMAL, AT CRUISE POWER OIL PRESSURE
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