Lycoming LTIO-540-J2BD
Service difficulty reports · 442
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 = 'LTIO540J2BD' 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 = 'LTIO540J2BD' 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 CA081112006Tube · flat(CAN) AFTER LANDING, IT WAS NOTICED THAT THE NOSEWHEEL WAS FLAT. DISASSEMBLY OF THE NOSEWHEEL HUB SHOWED A POSSIBLE WEAR SPOT BETWEEN THE TIRE AND TUBE. THE TUBE WAS DAMAGED DURING THE LANDING AND TAXI SO IT IS NOT KNOWN IF THIS WAS THE ACTUAL CAUSE OF THE PRSDR BSY2008F00002Clamp · failedAFTER TAKEOFF AT 4,000 FT RT ENGINE FAILED AND ACFT RETURNED WITH NO PROBLEMS. MAINT FOUND INDUCTION TUBE CAME OFF INTER-COOLER REDUCING MANIFOLD PRESSURE TO A NORMALLY ASPIRATED ENGINE. REPLACED WITH NEW DUCT AND CLAMP. (K)SDR CA080829006Torque Tube · corroded(CAN) DUE FOR INSP IAW SB 1105A, AWD 2003-24-07, EXTERNAL RUST FOUND. HOLE DRILLED IN TOP OF TUBE, SEVERE CORROSION FOUND ON LOWER INTERNAL SURFACES. PART REMOVED FROM SERVICE UNSERVICEABLEV.SDR CA080829004Pump · leaking(CAN) THE FUEL WAS FOUND DURING REGULAR INSP LEAKING, FUEL PUMP WAS REPLACED WITH SIMILAR ONE. THE PROBLEM DIDN’T AFFECT THE ENG PERFORMANCE. FUEL TRACE WAS LOCATED BETWEEN BODY STAGE OF THE PUMP. THIS IS THE FIRST PROBLEM OF LEAK WITH THIS TYPE.SDR CA080825004Clamp · faulty(CAN) FLIGHT CREW REPORTED ALL FLIGHT CONTROL TRIM AND BOTH ENGINE COWL FLAP INDICATORS INOP. MAINT INVESTIGATION ISOLATED THE VOLTAGE CLAMPER AT FAULT. AFTER REMOVAL OF FAULTY CLAMPER FOUND THE INTERNAL RESISTOR BADLY BURNED AND PARTIALLY MELTED. VOLTAGE CLAMSDR Z3O2008F00000Drive Gear · brokenPILOT REPORTS RT ENGINE WENT INTO FEATHER AND SHUT DOWN DURING FLIGHT, AFTER INSPECTION, FOUND RT GOVERNOR DRIVE GEAR SHEARED FROM GOVERNOR, THE THREE JOINTS THAT ATTACH THE DRIVE GEAR TO THE GOVERNOR HAD BEEN BROKEN OFF ALLOWING GEAR TO COME OUT. AFTER REVIEWSDR CA080825003Solenoid · failed(CAN) FLIGHT CREW REPORTED DURING SHORT FINAL, SELECTING THE FLAPS FROM 25 DEGREES TO 40 DEGREES, THE ACFT YAWED SEVERELY. VISUAL CHECK OF THE FLAP REVEALED THE LT FLAP AT FULL DOWN AND THE RT FLAP AT APPROX 25 DEGREES. THE ACFT LANDED WITHOUT FURTHER INCIDENTSDR 2008FA0000581Vernatherm · failedTHIS VERNATHERM HAD A SHAFT AND NUT ASSY THAT WAS SECURED WITH A ROLL PIN. THE SHAFT FAILED AT ROLLPIN. THE NUT, SHAFT PIECE AT ROLLPIN TRAVELED THRU THE OIL GALLY AND LODGED AT A FITTING. HIGH OIL TEMP ALERTED US TO THIS FAILURE, OIL PRESSURE WAS NORMAL.(KSDR CA080811007Plug · loose(CAN) WHILE ACCOMPLISHING REPETITIVE INSP (50HR) FOR AD2008-08-14, FOUND BOTH ENGINE FUEL SERVO PLUGS LOOSE. BOTH PLUGS REMOVED, INSPECTED, RETORQUED AND SAFETIED IAW AD REQUIREMENTS. NO ENGINE PERFORMANCE SNAGS REPORTED. LT ENGINE: TIO-540-J2BD S/N: L6203-61ASDR CA080714003Turbocharger · failed(CAN) RT TURBOCHARGER FAILED SHORTLY AFTER T/O. ENGINE SHUTDOWN AND ACFT RETURNED TO AIRPORT FOR AN UNEVENTFUL LANDING.SDR CA080623003Seal · leaking(CAN) DURING 2 ROUTINE INSP OF THE ENGINE, IT WAS DISCOVERED THAT THE CRANKSEAL WAS LEAKING. A NEW SEAL WAS INSTALLED AT APPROXIMATLEY 50 HRS. THE NEXT SCHEDULED INSP CARRIED OUT AT 98 HRS REVEALED THE SEAL LEAKING AGAIN. THE ENGINE WAS STILL UNDER WARRENTY ANSDR CA080630003Starter · failed(CAN) AFTER SITTING FOR 4 MONTHS, THE PILOT TRIED TO START THE ENGINE AND AFTER ONE REVOLUTION THE STARTER QUIT. THE STARTER WAS REMOVED AND REPLACED. THE ARMATURE END OF THE STARTER HSG WAS BROKEN OUT AND TWISTED, INDICATING THAT SOMETHING WAS BINDING IN THE SDR CA080619004Governor · malfunctioned(CAN) AFTER INSTALLATION OF THE OVERHAULED GOVERNOR, THE TEST FLIGHT WAS CARRIED OUT AND THE ENGINE WAS OVER SPED. THE GOVERNOR WAS SENT BACK TO THE REPAIR FACILITY, THE FACILITY REPORTS NOTHING ABNORMAL.SDR CA080619006Turbocharger · failed(CAN) AN OVERHAULED ENGINE COMPLETE WITH NEW TURBOCHARGER WAS INSTALLED. AFTER THE FIRST HOUR OF THE FLIGHT THE TURBOCHARGER COMPLETELY FAILED. MAINT INSTALLED A NEW TURBOCHARGER AND ACFT RETURNED TO SERVICE.SDR CA071207002Trunnion · cracked(CAN) DURING INSPECTION, A CRACK WAS FOUND IN THE RT UPPER TRUNNION, MOVING FROM THE BOTTOM OF THE TRUNNION UPWARDS TOWARD THE ATTACHMENT POINT, THE GEAR DOOR ROD. THIS IS THE SECOND ONE THIS YEAR. (TC NR 20071207002)SDR CA071015001Seat Belt · broken(CAN) AFTER STARTUP THE CAPTAIN WENT TO ATTACH AND TENSION HIS LAPBELT. AT THAT POINT THE LAP BELT DISCONNECTED FROM THE SEAT. CLOSER INSPECTION SHOWED CORROSION IN THE AREA OF THE BOLT HOLE OF THE FEMALE SIDE. THE SEATS ARE PROVIDED WITH A COVER OVER THIS ARESDR CA070928003Controller · leaking(CAN) DURING TAKEOFF A VIBRATION AND LOW EGT WAS FELT ON THE LT ENGINE. TAKEOFF POWER WAS STILL ACHIEVED FOR THE FLIGHT. THE AIRCRAFT RETURNED TO LAND. BOTH THE DENSITY AND DIFFERENTIAL CONTROLLERS WERE FOUND TO HAVE OIL LEAKS. THE OIL WOULD CONTAMINATE THE AISDR 2007FA0000501Main Bearing · delaminatedCUSTOMER FOUND METAL IN FILTER DURING ROUTINE MAINTENANCE. TOOK ENG. APART AND FOUND 2 CENTER MAIN BRGS. WHERE DELAMINATED.SDR FFS2007F00000Pump · leakingDURING A REGULAR SCHEDULED INSPECTION, IT WAS NOTED THAT THE RT ENGINE DRIVEN FUEL PUMP WAS LEAKING. THE PUMP WAS LEAKING FROM THE PRESSURE DOME HOUSING GASKETS. (K)SDR CA070420002Bolt · failed(CAN) BOLT FAILED CAUSING CONNECTING ROD TO BECAME DETACHED FROM CRANKSHAFT CAUSING MAJOR DAMAGE TO LOWER END OF ENGINE. (TC NR 20070420002)SDR CA070223003Seal · leaking(CAN) DURING A NORMAL WALK AROUND, OIL WAS OBSERVED ON THE COWLING. AN INVESTIGATION INTO THE OIL LEAK REVEALED THE CRANKSHAFT SEAL WAS BLOWN OUT. THE OIL SUMPS WERE DRAINED AND OIL FILTER CHECKED AND FOUND TO CONTAIN LARGE QUANTITIES OF METAL FILINGS. THE ENGSDR 07006Hose · brokenPILOT NOTICED A DECREASE IN MANIFOLD PRESSURE ON THE RT ENGINE. LANDED AIRCRAFT, AND CALLED DOM FOR INSTRUCTIONS. MAINTENANCE FOUND UPPER DECK PRESSURE HOSE BROKEN. NEW HOSE WAS INSTALLED. RAN AND OPS, CHECKED GOOD.SDR DGCA0707006Hose · brokenPILOT NOTICED A DECREASE IN MANIFOLD PRESSURE ON THE RT ENGINE. LANDED AIRCRAFT, AND CALLED DOM FOR INSTRUCTIONS. MAINTENANCE FOUND UPPER DECK PRESSURE HOSE BROKEN. NEW HOSE WAS INSTALLED. RAN AND OPS, CHECKED GOOD.SDR 2006FA0001129Keeper · brokenFOUND VALVE KEEPER BROKEN ON ROUTINE VALVE INSPECTION IAW SB 388C. (K)SDR 2006FA0001130Keeper · brokenFOUND NR 6 CYLINDER VALVE KEEPER BROKEN ON ROUTINE VALVE INSPECTION IAW SB 388C. (K)SDR CA061004006Bearing · broken(CAN) THE AIRCRAFT DEPARTED THE RUNWAY FOR A 1 HOUR TRIP. APPROXIMATELY 17 MINUTES INTO THE CRUISE PORTION OF FLIGHT THE PILOT NOTICED A LOSS IN OIL PRESSURE FOLLOWED BY NOISE FROM THE RT ENGINE. THE PILOT IMMEDIATELY FEATHERED THE PROP AND SHUTDOWN THE ENGINESDR BSYA200600024Wastegate Valve · lack of lubeRIGHT WAS SURGING AFTER TAKEOFF, RETURNED TO BASE BUF. MAINTENANCE LUBED TURBOCHARGER WASTE GATE, GROUND RUN GOOD.SDR BSYA200600023Magneto · failedON TAKEOFF OUT OF PHL, LEFT ENGINE STARTED SURGING RETURNED TO BASE WITH NO PROBLEMS. MAINTENANCE FOUND THE LEFT MAGNETO DEAD. REMOVED AND REPLACED MAGNET, OPS CHECKS GOOD.SDR WVB2006F00002Oil System · unknownPILOT NOTICED RT ENGINE OIL PRESSURE DROP AFTER CLIMBING THRU 24000 FT. HE SHUT THE ENGINE DOWN AS A PRECAUTIONARY MEASURE. THE PILOT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE COMPLIED WITH A VISUAL CHECK OF THE ENGINE AND DID A FULL ENGINE RUN UP. THE SDR BSYA200600019Pump · malfunctionedON TAKEOFF OUT OF BUF RIGHT ENGINE WANTED TO QUIT. PILOT ABORTED TAKEOFF. MAINTENANCE FOUND FUEL PRESSURE LOW AND ENGINE WOULD NOT IDLE. CHANGED BOTH THE ENGINE DRIVE FUEL PUMP AND FUEL SERVO, OPS CHECKS GOOD.SDR ENHA2006P3103Engine · power lossPILOT REPORTS AFTER ESTABLISHING CRUISE, NOTICED OIL PRESSURE DROPPING, RT ENGINE AND ALSO A LOW FREQUENCY VIBRATION. PERFORMED (LOW OIL PRESSURE) CHECKLIST PROCEDURE AND SECURED ENGINE. (K)SDR ENHA2006P3102Cylinder · leakingON CLIMB RT ENGINE MANIFOLD PRESSURE REDUCED TO AMBIENT, UPON LANDING, NOTICED OIL LEAKAGE AND STREAKING RT N COWLING. REPLACED CYL NR 2. AC RETURNED TO SERVICE. (K)SDR 2006F00023O-Ring · failedDURING T/O LARGE AMOUNT OF SMOKE VISIBLE. PILOT SHUT DOWN RIGHT ENGINE RETURNED TO LAND. MAINTENANCE NOTED A PIECE OF O-RING MISSING ON OIL FILLER CAP WHICH SPEWED OIL OVER EXHAUST AND TURBO. REPLACED OIL CAP O-RING AND PROBLEM FIXED.SDR FFS2006F00001Bearing Seal · failedABORTED TAKEOFF AT HOME AIRPORT DUE TO DECREASE IN POWER DURING DEPARTURE. (K)SDR CA060118004Pushrod · chafed(CAN) CYLINDER BAFFLE TIE ROD P/N 71562-03 WAS FOUND WITH A SECURING INTER CYLINDER BAFFLE, ADEL CLAMP MISSING. THIS HAD ALLOWED THE BAFFLE TIE ROD TO RAISE UP TO THE POINT WHERE IT CAME INTO CONTACT WITH THE LOWER SIDE OF THE NR 4 CYLINDER EXHAUST PUSH ROD TUSDR AU510001898Regulator · leakingCABIN HEATER FUEL PRESSURE REGULATOR LEAKING FUEL FROM DIAPHRAGM.SDR AU510001995Camshaft · wornRT ENGINE METAL CONTAMINATION. INVESTIGATION FOUND CAMSHAFT LOBE FOR INLET VALVE ON NR 5 AND NR 6 CYLINDERS FAILED/WORN.SDR 2005FA0001562Valve Seat · separatedVALVE SEAT SEPARATED FROM CYLINDER. (K)SDR ENHA2005PA310Pump · malfunctionedIN FLIGHT RT ENG SHUTDOWN. PILOT ATTEMPT AIR RESTART, UNABLE TO AIR START, SECURED ENG, LANDED, 1 ENG OPERATING. OBSERVED FUEL STREAMING OFF OF RT WING, OBSERVED FUEL IND (QTY) DROPPING FASTER THAN LT IND, R ENG SPUTTERED, SHUTDOWN. NO EVIDENCE OF FUEL LEAKASDR AU510001444Bypass Valve · disintegrated(AUS) RH ENGINE OIL BYPASS VALVE (VERNATHERM) BREAKING UP IN AREA OF CIRCLIP RING. METAL CONTAMINATION OF OIL SYSTEM. (OTHER CAUSE: MATERIAL ) (CASA# 510001444)SDR AU510001634Hose · fracturedRT ENGINE SUMP TO DIFFERENTIAL PRESSURE CONTROLLER FAILED. HOSE IS MANUFACTURED FROM 306 RUBBER AND IT IS SUSPECTED THAT THE MATERIAL IS INCAPABLE OF WITHSTANDING HIGH TEMPERATURES. ORIGINAL PIPER HOSE P/N 39999-14.SDR MK92005F00000Stud · destroyedTHE FORWARD EXHAUST STUD BECAME LOOSE AND WAS FORCED OUT OF POSITION BY THE EFFECTS OF EXHAUST PRESSURES WORKING AGAINST IT. WHEN THE THREADS WERE COMPLETELY DESTROYED, BOTH ON THE STUD AND IN THE CYLINDER HEAD, THE EXHAUST WAS ALLOWED TO EXIT THE HEAD FROM ASDR CA050610002Fork · cracked(CAN) DURING A WALKAROUND THE PILOT NOTICED THE BRAKE DISC WAS RUBBING AGAINST THE SIDE OF THE GEAR FORK. AFTER THE WHEEL ASSEMBLY WAS REMOVED A CRACK WAS FOUND ON THE AXLE AT THE INNER MOST BEARING RIDE LOCATION. THE CRACK WAS MORE THAN A THIRD OF THE WAY ASDR BSYA200500010Bearing · wornON TAKEOFF OUT OF BUF TOWER NOTICED A LOT OF SMOKE, PILOT ABORTED TAKEOFF AND WAS TOWED BACK. MAINTENANCE FOUND BEARING GONE IN THE TURBO CHARGER AND OIL LEAKING INTO THE EXHAUST. REMOVED AND REPLACED TURBO CHARGER, OPS CHECKS GOOD.SDR CA050516009Hose · leakingDURING THE LANDING APPROACH, THE GEAR WOULD NOT COME DOWN AND LOCK. AN EMERGENCY EXTENSION WAS CARRIED OUT USING THE HANDPUMP. AFTER LANDING AN INSPECTION OF THE NOSE GEAR AREA SHOWED A LOT OF HYDRAULIC FLUID LEAKING. THIS WAS TRACED TO THE NOSE GEAR ACTUATSDR AU510001723Shaft · brokenRT ENGINE TURBOCHARGER MAIN SHAFT BROKEN. ENGINE HAD JUST BEEN FITTED FOLLOWING OVERHAUL AND AIRCRAFT WAS ON ACCEPTANCE FLIGHT.SDR AU510001614Tailpipe · cracked(AUS) RT ENGINE TURBOCHARGER TAILPIPE CRACKED FOR APPROX 90 PERCENT OF CIRCUMFERENCE. TAILPIPE ALSO CONTAINED 3 HOLES RANGING IN DIAMETER FROM 12.7 MM TO 25.4MM (0.5IN TO 1IN). (CASA NR 510001614)SDR AU510001731Link · cracked(AUS) LINKAGE CRACKED. FOUND DURING INSPECTION IAW MFG SL 1088. (AD/SB DESC: MFG SL 1088 ) (CASA NR 510001731).SDR CA050228009Crankcase · cracked(CAN) SUSPECT CRACK IN THE VICINITY OF CYLINDER NR 2. ENGINE REMOVED FOR FURTHER INSPECTION.SDR AU510001810Turbocharger · failedRT ENGINE TURBOCHARGER FAILED.
Back to Lycoming LTIO-540-J2BD