Continental TSIO-360-EB
Service difficulty reports · 76
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 = 'TSIO360EB' 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 = 'TSIO360EB' 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 CA990202002Vibrator · failed(CAN) CABIN HEATER STARTED BACKFIRING AND PILOT SMELLED ODOR. HEATER TURNED OFF. BANGING AND ODOR STOPPED. HEATER REMOVED AND IGNITION FOUND INTERMITTENT. VIBRATOR REPLACED.SDR CA981230013Bracket · cracked(CAN) AFTER READING FEED-BACK 1/98 OF NOSE LANDING GEAR ATTACH, IT WAS NOTED THAT ATTACH POINT AND FIREWALL MOVED WHEN FORCE APPLIED. INSPECTION FOUND THE STABILATOR PULLEY BRACKET WAS CRACKED AND THE RIVETS SHEARED WHICH ATTACH THE NOSE GEAR MOUNT FITTING. SDR 98ZZZX3936Valve · failedDURING AIRCRAFT INSPECTION, INSPECTORS FOUND NEITHER ENGINE FUEL SHUT-OFF VALVE WOULD SHUT OFF FUEL TO ENGINES. TEAR DOWN INSPECTION REVEALED O-RINGS IN VALVES IN SHREADS. INSTALLED NEW SEAL MODIFICATION KITS AND REINSTALLED VALVES. OPS CHECK OK. SUBMITTERSDR 98ZZZX3937Valve · failedDURING AIRCRAFT INSPECTION, INSPECTORS FOUND NEITHER ENGINE FUEL SHUT-OFF VALVE WOULD SHUT OFF FUEL TO ENGINES. TEAR DOWN INSPECTION REVEALED O-RINGS IN VALVES IN SHREADS. INSTALLED NEW SEAL MODIFICATION KITS AND REINSTALLED VALVES. OPS CHECK OK. SUBMITTERSDR 99ZZZX580Valve · failedINTAKE VALVE SEAT CAME LOOSE, STUCK UNDER VALVE. CYLINDER CERMINIL STEEL (EC) ENG T.W. SMITH OVERHAULED. PART TIME 102.8 HRS. AIRCRAFT LANDED RESTARTED, WOULD NOT DEVELOP POWER.SDR BIER9802050Condensor · shortedPILOT REPORTED, EXCESS RPM DROP ON RUN-UP, INSP OF MAG INTERNALS REVEALED TOP OF CONDENSOR, WHERE WIRE IS SOLDERED TO CONDENSOR WAS CONTACTING MAG CAP. IT HAD FINALLY WORN THROUGH THE INSULATING PAINT AT THE TOP. SUBMITTER STATES, THE SOLDER JOINT AND WIRE WSDR 97ZZZX3677Bearing · failedMAGNETIC RETRIEVAL TOOL PRODUCED A METAL PIECE, .870 INCH BY .210 INCH BY .100 INCH FROM CRANKCASE SUMP. INVESTIGATION DISCLOSED NR 3 MAIN BEARING WAS LOOSE IN CRANKCASE AND WAS THE SOURCE OF THE METAL FRAGMENT. DISASSEMBLY SHOWED NR 2 MAIN BEARING WAS WORKISDR 97ZZZX3686Gear · wornGOVERNOR WAS REMOVED DURING CRANKCASE REPAIR. GOVERNOR DRIVE GEAR TEETH WERE WORN AWAY 75 PERCENT. GOVERNOR DRIVEN GEAR INTERNAL SPLINES WERE WORN 25 PERCENT. FUEL PUMP SPLINES ON SAME GEAR WERE NOT WORN. CAMSHAFT WAS WORN .025 INCH ON DIAMETER THAT PN 6295SDR 97ZZZX3687Camshaft · gear wornGOVERNOR WAS REMOVED DURING CRANKCASE REPAIR. GOVERNOR DRIVE GEAR TEETH WERE WORN AWAY 75 PERCENT. GOVERNOR DRIVEN GEAR INTERNAL SPLINES WERE WORN 25 PERCENT. FUEL PUMP SPLINES ON SAME GEAR WERE NOT WORN. CAMSHAFT WAS WORN .025 INCH ON DIAMETER THAT PN 6295SDR 97ZZZX3688Gear Spline · wornGOVERNOR WAS REMOVED DURING CRANKCASE REPAIR. GOVERNOR DRIVE GEAR TEETH WERE WORN AWAY 75 PERCENT. GOVERNOR DRIVEN GEAR INTERNAL SPLINES WERE WORN 25 PERCENT. FUEL PUMP SPLINES ON SAME GEAR WERE NOT WORN. CAMSHAFT WAS WORN .025 INCH ON DIAMETER THAT PN 6295SDR 97ZZZX3704Relief Spring · wornACCESSORY CASE WAS PARTIALLY DISASSEMBLED FOR CLEANING DURING MAJOR ENGINE REPAIRS. OIL PRESSURE RELIEF VALVE SPRING WAS WORN ON OUTSIDE OF COILS WHERE THEY RIDE ON INSIDE OF RELIEF VALVE PLUNGER. COILS WERE WORN TO .034 INCH FROM .050 INCH NEW DIAMETER. THSDR CA970212003Link Assy · broken(CAN) AIRCRAFT WAS ON A PILOT TRAINING FLIGHT. PILOT SELECTED GEAR DOWN AND THE SYSTEM INDICATED DOWN AND LOCKED. 3 GREEN AND VISUAL IDENT THROUGH THE SIDE MIRROR. UPON TOUCHDOWN THE NOSE GEAR COLLAPSED. AWAITING FURTHER INFORMATION.SDR 97ZZZX181Stud · stretchDURING THE COURSE OF A NORMAL ENG OVERHAUL, IT WAS FOUND THAT ABOUT ONE-THIRD OF THE CYL DECK STUDS WOULD NOT HOLD SPECIFIED TORQUE WITHOUT STRETCHING. THE STUDS ARE A NEWER 'NECKED DOWN' DESIGN. THE MECH REPLACED ALL CYL DECK STUDS WITH AN OLDER STRAIGHT DESDR 96ZZZX5904Engine · roughnessUPON ROTATION, ENGINE ROUGHNESS WAS NOTED BY PILOT. TOWER REPORTED SMOKE FROM RIGHT ENGINE. LANDING PATTERN WAS ENTERED IMMEDIATELY, AND UNEVENTFUL LANDING MADE. MAINTENANCE COULD NOT DUPLICATE PROBLEM ON GROUND. RUN-UPS AND ENGINE INSPECTIONS SHOWED NO VISDR 96ZZZX5713Pump · failedENGINE DRIVEN FUEL PUMP DEVELOPED EXCESSIVE OUTPUT. (HIGH PRESSURE) FOUND FUEL IN DECK REFERENCE LINE, INDICATING INTERNAL LEAKAGE.SDR 96ZZZX4151Valve · leakingFUEL MANIFOLD VALVE HAS FUEL LEAKING FROM TOP OF UNIT. INCREASE TORQUE VALUE FOR SCREWS.SDR 96ZZZX4157Turbocharger · locked upPILOT APPLIED POWER TO RIGHT ENGINE FOR PRE-FLIGHT CHECK. ENGINE WOULD ONLY TURN UP TO 26 INCHES MAN/PRESSURE. FOUND TURBO HAD LOCKED UP. INSTALLED OVERHAULED TURBO, ENGINE GROUND RAN, CHECKED NORMAL. AIRCRAFT TEST FLOWN, ALL CONDITIONS NORMAL.SDR 96ZZZX3869Crankcase · crackedTHE INSPECTION FOUND CRANKCASE HAS A SMALL .3750 INCH CRACK NEXT TO THE UPPER BOLT JUST FORWARD OF CYLINDER NR 5. THIS IS CONSIDERED A NON-CRITICAL AREA PER SB M90-17.SDR 96ZZZX2762Impulse Coupler · cam splitMAGNETO IMPULSE COUPLER CAM SPLIT IN HALF DURING RE-INSTALLATION ON MAGNETO DURING MAGNETO 500-HOUR INSPECTION AND IMPULSE COUPLER AD 78-09-07R3.SDR 96ZZZX2510Crankcase · crackedSMALL CRACK FOUND IN RIGHT SIDE OF CRANKCASE NEXT TO THROUGH-BOLT JUST FORWARD OF CYLINDER NR 5. CONSIDERED NON-CRITICAL AREA PER SB M90-17.SDR 96ZZZX2068Clutch Spring · failedCLUTCH SPRING WOUND ITSELF AROUND STARTER SHAFT GEAR AND WOULD NOT ALLOW ENGINE TO START.SDR CA960416001Piston Pin · fractured(CAN)ENGINE TEARDOWN DUE TO METAL CONTAMINATION OF THE OIL. #4 PISTON DISINTEGRATED DUE TO FRACTURE OF PISTON PIN. MAGNAFLUX REVEALS STRESS CRACKING IN ANOTHER PIN.SDR 96ZZZX1122Magneto · clamp brokenCOIL CLAMP FOUND BROKEN AT BEND RADIUS DURING MAGNETO 500-HOUR INSPECTION. NOTE: CLAMP HAD WHITE DYKEM MARK PER TCM MANUAL PAGE 7-6, PARAGRAPH 7.2.G(D).SDR 95ZZZX6416Through Bolt · brokenCRANKCASE 'THROUGH' BOLTS, UPPER AND LOWER FOR NR 2 AND NR 3 CYLINDERS, BROKEN AT CYLINDER BASE NUTS. LOCATED AFTER REPORTED OIL LEAK. ENGINE TT 3,816.90 HOURS. TSMOH, 535.63 HOURS.SDR 95ZZZX5030Distributor Blk · crackedDURING A MAGNETO 500-HOUR INSPECTION, ONE MOUNTING HOLE FOR THE DISTRIBUTER BLOCK WAS FOUND CRACKED.SDR 95ZZZX5031Distributor Blk · crackedDURING MAGNETO 500-HOUR INSPECTION, ONE MOUNTING HOLE OF THE DISTRIBUTOR BLOCK WAS FOUND CRACKED.
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