Continental TSIO-360-F
Service difficulty reports · 28
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 = 'TSIO360F' 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 = 'TSIO360F' 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 2012FA0000228Spark Plug · damagedPILOT REPORTED ENGINE BEGAN RUNNING ROUGH AT 11,000 FT. DESCENDED TO 5,000 FT AND ENGINE OPERATED CORRECTLY. RETURNED TO AIRPORT, LANDED WITHOUT FURTHER INCIDENT. REMOVED TOP COWLING AND ALL 12 SPARK PLUGS, PN RMH38E. ALL SPART PLUGS RUSTED ON OUTSIDE AND SDR CA090303006Main Bearing · failed(CAN) LARGE PIECE OF FERROUS MATERIAL FOUND IN OIL PICKUP SCREEN DURING ROUTINE INSP, PIECE IDENTIFIED AS PORTION OF CTR MAIN BRG. ENGINE REMOVED FROM ACFT, DISASSEMBLED, INSP CONFIRMS COMPLETE FAILURE OF NR 2 CTR MAIN BRG. IN CONJUNCTION, CRANKCASE BRG SADDLSDR CA090220005Plug · missingON APPROACH TO YBL, THE PILOT DETECTED BURNING OIL AND SAW SMOKE, THE PILOT LANDED THE AIRCRAFT AND NOTICED A LARGE AMOUNT OF OIL ON THE BELLY OF THE AIRCRAFT AND DRIPPING FROM THE COWLS, AFTER THE TECHNICIAN INVESTIGATED THE OIL LEAK HE FOUND A HOLE WHERE A PSDR NTB2008F00000Impulse Coupling · brokenIMPULSE COUPLING SPRING BROKEN. EVIDENCE OF PRE-EXISTING CRACK AND CORROSION. VERY LOW TIME IN SERVICE. MAG TO ENGINE TIMING LOST. BOTH MAGS EXPERIENCED THE SAME FAILURE ALMOST SIMULTANEOUSLY. (K)SDR NTB2008F00001Spring · brokenIMPULSE COUPLING SPRING BROKEN. EVIDENCE OF PRE-EXISTING CRACK AND CORROSION. VERY LOW TIME IS SERVICE. MAG TO ENGINE TIMING LOST. BOTH MAGS EXPERIENCED THE SAME FAILURE ALMOST SIMULTANEOUSLY. (K)SDR CA070919001Tube · broken(CAN) FUEL DISCHARGE TUBE BROKE, ENGINE LOST POWER. SUSPECT MID-TUBE CLIP P/N: 626477-2 MAY HAVE FAILED FIRST. (TC NR 20070919001)SDR CA070502008Control Cable · damaged(CAN) MIXTURE CONTROL WAS FOUND TO BE STIFF BY MAINT ON AN ENGINE START FOR TAXI TO HANGER. CABLE WAS REMOVED. THE CABLE ROUTING POSITIONS THE CABLE LESS THAN (6) INCHES FROM THE TURBOCHARGER. AN ASBESTOS COVER HAD PREVIOUSLY BEEN PLACED OVER THE CABLE AND STISDR CA070118003Pump · faulty(CAN) ENGINE DRIVEN FUEL PUMP OUTPUT IS LOW AT RATED RPM 2600. (TC NR 20070118003)SDR 2004FA0000845Shaft · mismanufacturedDURING 100 HOUR INSP AT 1V5, LT CONTROL COLUMN, P/N 62834-02, WAS REMOVED FOR REPLACEMENT DUE TO EXCESS PLAY. UPON REMOVAL, CONTROL COLUMN SHAFT, P/N 62716-02, WAS FOUND TO BE DRILLED (FOR AN-386-1-6A TAPER PIN) LESS THAN 0.025 INCH FROM AFT END OF SHAFT. HOLSDR 2004FA0000846Shaft · mismanufacturedDURING 100 HR INSP AT 1V5, LT CONTOL COLUMN UNIVERSAL,P/N 62834-02, WAS REMOVED FOR REPLACEMENT DUE TO EXCESS PLAY. CONTROL COLUMN SHAFT, P/N 62716-02, WAS FOUND TO BE DRILLED (FOR THE AN-386-1-6A TAPER PIN) LESS THAN 0.025 INCH FROM AFT END OF SHAFT. HOLE ISDR AUS20030626Stud · cracked(AUS) MAIN LANDING GEAR SIDE BRACE STUD CONTAINED LONGITUDINAL MPI INDICATIONS. FOUND DURING INSPECTION IAW AD/PA28/91 AMDT1.SDR AUS20030367Link · failed(AUS) NOSE LANDING GEAR DRAG LINK ASSEMBLY SHEARED IN AREA LOCATEDFORWARD OF THE RH ATTACHMENT POINT.SDR AUS20020155Capacitor · faulty(AUS) LH MAGNETO CAPACITOR WIRE INTERMITTENT CONTACT.SDR AUS20020156Capacitor · faulty(AUS) RH MAGNETO CAPACITOR WIRE INTERMITTENT CONTACT.SDR AU000534Stud · cracked(AUS) LEFT AND RIGHT MAIN LANDING GEAR SIDE BRACE STUDS CRACKED. FOUND DURING MAGNETIC PARTICLE INSPECTION IAW AD/PA28/91. (X)SDR CA000530031Trunnion · cracked(CAN) DURING A 50-HOUR INSPECTION OF THE LANDING GEAR, THE NOSE GEAR TRUNNION WAS FOUND CRACKED AT SHIMMY DAMPENER ATTACHMENT POINT. POSSIBLE CAUSE - OVERSTEER.SDR AU000342Fuel Tank · leaking(AUS) FUEL TANK LEAKING. INSPECTION FOUND FAULTY SEALANT. FOUND FOLLOWING COMPLIANCE WITH AD/GEN/80.SDR 99ZZZX1076Bypass Pipe · not installedA TURBO HEAT BLANKET WAS INSTALLED ON 1-28-99. SUBMITTER STATED DURING THE INSTALLATION OF THE TURBO HEAT BLANKET, THE MECHANIC FAILED TO REINSTALL THE EXHAUST BYPASS VALVE PIPE (STC SA4731 NM/STC 4731 NM) THAT DIRECTED EXHAUST GAS OUTBOARD OF THE ENGINE. THSDR CA990318049Flyweight · loose(CAN) PILOT REPORTED ROUGH RUNNING ENGINE ON RUN-UP. INSPECTION FOUND RIGHT HAND MAGNETO DEAD. DURING REMOVAL OF THE MAGNETO, THE IMPULSE COUPLING FLYWEIGHT FELL OUT. THE AXLE/RIVET HEAD FOUND MISSING. ALL CYLINDERS, OIL SUMP AND ACCESSORY SECTION, WERE INSDR CA980430038Tube Assy · cracked(CAN) TUBE CRACKED UNDER CLAMP. NOT VISIBLE WITH CLAMP ON. REPLACED.SDR CA980331021Cable · stiff(CAN) BOTH PROP AND MIXTURE CONTROL CABLES VERY STIFF. AREA BEHIND TURBO BADLY CORRODED. CABLES REPLACED.SDR AU970577Elt · faulty(AUS) ELT FAULTY - `G' SWITCH UNSERVICEABLE - BATTERIES OF EUROPEAN ORIGIN FITTED - BATTERY INSULATORS WORN - EVIDENCE OF MOISTURE INGRESSSDR AU970450Cable · stuck(AUS) MIXTURE CONTROL CABLE STUCK - CABLE RUNS ADJACENT TO TURBOCHARGER - THROTTLE CABLE AND PROPELLER CONTROL CABLES ALSO RUN ADJACENT TO THE TURBOCHARGERSDR 97ZZZX1589Cylinder · head separatedDURING ANNUAL INSPECTION, FOUND NR 2 CYLINDER HEAD SEPARATING FROM BARREL. THE HEAD WAS TURNED COUNTERCLOCKWISE 4 DEGREES AND WAS .0625 INCH FARTHER FROM FIRST CYLINDER FIN THAN OTHER CYLINDERS. LEAK CHECK (PARAGRAPH C TCM SB 96-12) REVEALED LEAK. COMPRESSISDR AU970140Actuator · failed(AUS) NOSE LANDING GEAR HYDRAULIC ACTUATOR FAILED AT FUSELAGE ATTACHMENT POINTSDR 97ZZZX3739Stud · failedAS A RESULT OF AN ACCIDENT, FOLLOW-UP INVESTIGATION REVEALED THE ENGINE LOST POWER DUE TO FAILURE OF THE ROCKER ARM SHAFT HOLD-DOWN STUDS ON NR 2 CYLINDER. AD 92-04-09 WAS C/W. THE CYLINDER WAS AN EXCHANGE INSTALLED AT THE LAST OVERHAUL. STUDS FAILED MOST LSDR 96ZZZX5470Lock Tab · failedCYLINDERS WERE SENT OUT FOR CHROMING AND OVERHAUL. CYLINDERS WERE RECEIVED BACK READY TO INSTALL. NEW SUPERIOR AIR PARTS ROCKER ARM SHAFT BOLT LOCK TABS WERE INSTALLED. UPON BENDING TANGS OVER BOLT HEADS, ALL TANGS EITHER CRACKED OR BROKE OFF COMPLETELY. SSDR 95ZZZX5104Piston Pin · brokenNR 2 CYLINDER PISTON PIN FAILED AT MIDSECTION (BROKEN IN HALF). SUBSEQUENT FAILURE OF NR 2 PISTON AND METAL CONTAMINATED SUPERIOR AIR PARTS SUPPLIED PISTON PIN WITH A SHIP DATE OF 11-8-94. CAUSE UNKNOWN.
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