Continental TSIO-360-CB
Service difficulty reports · 17
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 = 'TSIO360CB' 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 = 'TSIO360CB' 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 2015FA0000439Engine · failedAFTER TAKEOFF, IN CRUISE FLIGHT AT 7,000' ASL, FRONT ENGINE OIL PRESSURE DROPPED TO LOWER RED-LINE LIMIT, OIL TEMPERATURE WAS NORMAL APPROXIMATELY 150F AND ENGINE RUNNING SMOOTHLY. WITHIN 10 SECONDS, ENGINE WENT FROM SMOOTH RUNNING CONDITION TO A LOSS OF 300-SDR YYE2008F00000Pump · failedTHE PRIMARY ELECTRIC/ HYD LANDING GEAR PUMP FAILED. THE ATTEMPT TO LWR THE GEAR WITH THE MANUAL GEAR LEVER ALSO FAILED, RESULTING IN A GEAR UP LANDING. THE PRIMARY PUMP FAILURE MAY HAVE CAUSED THE MANUAL PUMP FAILURE. (K)SDR JNE2008F00000Starter · failedINSTALLED TWO FACTORY ENGINES. AFTER SEVERAL TEST RUNS , THE FRONT STARTER SOLENOID FAILED ON. REPLACED THE SOLENOID WITH AN NEW MFG SOLENOID. ON A TEST FLIGHT ELECTRICAL FAILURE OCCURRED. IT HAPPENED BECAUSE OF AN OVERLOAD OF THE BATTERY AND ELECTRICALSYSTSDR 2005FA0000812Landing Gear · vibratesSEVERE NOSE GEAR SHIMMY DURING LANDING. NOSE GEAR STRUT SERVICED WITH MIL-H-5606, REQUIRED 30-WT FORK OIL. NEXT FLT A SEVERE SHIMMY AGAIN. INSP REVEALED ENG MOUNT BROKEN 6 PLACES AS A RESULT. ENG MOUNT & NOSE GEAR STRUT REPLACED, ON NEXT FLT, A SEVERE NOSESDR CA041108007Cable · frayed(CAN) AT INSPECTION THE AUTOPILOT ROLL SERVO BRIDLE CABLE WAS FOUND TO BE FRAYED WHERE IT RUNS OVER IT'S PULLEYS.SDR CA040930002Skin · cracked(CAN) DURING INSPECTION, CRACKS WERE DISCOVERED AT THE IB END OF THE LT AND RT UPPER OB WING SKINS WHERE THEY UNDERLAP THE FUEL TANK BAY COVERS. THE CRACKS ARE LOCATED IN THE RADIUS OF CUTOUT AREAS IN THE SKINS WHERE THE STINGERS JOIN AT WING STATION 150.0. TSDR 2004FA0000397Impulse Coupling · brokenPILOT REPORTED REAR ENGINE WAS HARD TO START. AFTER TROUBLESHOOTING, THE LT MAGNETO WAS REMOVED. UPON INSPECTION THE IMPULSE COUPLING WOULD NOT ROTATE IN THE CORRECT DIRECTION. THE MECH WAS NOT SURE IF WRONG IMPULSE COUPLING OR SPRING TURN BACKWARD. DUE TOSDR CA040122002Control Cable · frayed(CAN) DURING INSPECTION IT WAS DICOVERED THAT THESE CABLES (2EA. 1 LT AND 1 RT) WERE FRAYED WHERE THE CABLE BENDS AROUND THE FLAP CABLE QUADRANT LOCATED IN THE WING TRAILING EDGE.SDR CA040122003Control Cable · frayed(CAN) DURING INSPECTION IT WAS DISCOVERED THAT THESE CABLES (2EA. 1 LEFT AND 1 RIGHT) WERE FRAYED WHERE THE CABLE BENDS AROUND THE FLAP CABLE QUADRANT LOCATED IN THE WING TRAILING EDGE.SDR CA031119004Coupling · separated(CAN) COUPLING SEPARATED FROM TURBOCHARGER COMPRESSOR HOUSING CAUSING INDUCTION LEAK AND RESULTING POWER LOSS.SDR 2003FA0000433Turbocharger · misinstalledTURBOCHARGER UNABLE TO BOOST MANIFOLD PRESSURE. REMOVED TURBOCHARGER AND FOUND EXCESSIVE CLEARANCE BETWEEN T-WHEEL AND HOT SECTION HOUSING. INCORRECT PARTS ASSEMBLED INTO A COMPLETE UNIT. INSPECT PRODUCT PRIOR TO RELEASING TO SERVICE.SDR CA991229039Propeller · corroded(CAN) PROPELLER SEIZED DUE CORROSION.SDR 2000ZZZX364Crankshaft · crackedFOUND CRANKSHAFT FLANGE CRACKED (APPROXIMATELY 2.5 INCHES) ON BACK SIDE. ENGINE IS A FACTORY REBUILT WITH 48 HOURS AND NO RECORDED DAMAGE HISTORY. ENGINE INSTALLED IN REAR POSTION.SDR CA980811015Cylinder · separated(CAN) DURING FLIGHT, THE PILOT HEARD A LOUD NOISE, COMING FROM THE REAR ENGINE, FOLLOWED BY A DROP IN MANIFOLD PRESSURE AND ON LANDING A REDUCTION IN OIL PRESSURE. THE ENGINE SHUTDOWN ON THE RUNWAY. INSPECTION FOUND THE NR 4 CYLINDER SPLIT AT THE BARREL.SDR 96ZZZX700Valve Guide · excess wearFREQUENT FINDING OF LOW COMPRESSION ON EITHER FRONT OR REAR ENGINE WITH ONLY 808 HOURS TT. EACH TIME REPAIR WAS ACCOMPLISHED DUE TO THIS HISTORY, COMPLETE CYLINDER TEAR DOWN REVEALED EXCESS WEAR TO EXHAUST VALVES AND EXHAUST VALVE GUIDES. SUBMITTER SUSPECTS SDR 96ZZZX701Valve · excess wearFREQUENT FINDING OF LOW COMPRESSION ON EITHER FRONT OR REAR ENGINE WITH ONLY 808 HOURS TT. EACH TIME REPAIR WAS ACCOMPLISHED DUE TO THIS HISTORY, COMPLETE CYLINDER TEAR DOWN REVEALED EXCESS WEAR TO EXHAUST VALVES AND EXHAUST VALVE GUIDES. SUBMITTER SUSPECTS SDR 95ZZZX6536Crankshaft · crackedENGINE WAS WINDMILLING DURING A GEAR-UP LANDING (10-11-95) AT ROCKY MOUNTAIN AIRCARE. REPAIRED BELLY AND HAD PROP OVERHAULED AT H & H. REINSTALLED PROPELLER WITH A DIAL INDICATOR RUN-OUT CHK ONLY, WAS RETURNED TO SERVICE AS AIRWORTHY. DURING THE INSPECTION,
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