Continental TSIO-360-E
Service difficulty reports · 37
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 = 'TSIO360E' 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 = 'TSIO360E' 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 CA131121009Shimmy Dampener · broken(CAN) DURING A WALK AROUND, THE STUDENT PILOT NOTED THE SHIMMY DAMPENER AT AN AWKWARD ANGLE. THE SHAFT WAS BROKEN NEXT TO THE ROD END. NO OTHER VISIBLE DAMAGE WAS EVIDENT. THE PART WAS REPLACED.SDR 2012FA0000230Link Assy · brokenON LANDING, LINK ASSY ON MAIN GEAR TRUSS ASSY BROKE AT STRUT ATTACHMENT AREA, CAUSING ACFT TO VEER OFF RUNWAY.SDR APC2010F00000Bolt · brokenON PREFLIGHT, THE PILOT FOUND THE STABILATOR TO BE EXTREMELY LOOSE AND NOTIFIED MX. WHEN REMOVED TAIL CONE FOUND A BROKEN BOLT ON THE RT THAT HAD BACKED OUT. IMMEDIATELY GROUNDED THE WHOLE FLEET UNTIL SUCH TIME AS WE COULD INSPECT ATTACHING POINTS, BEARINGS SDR 2007FA0000547Pulley Bracket · chafedROLL SPOILER CABLE PN:S3779-4P233.7M WAS ROUTED INCORRECTLY OVER LOW FRICTION PULLEY P/N:S3504-4.5 (THROUGH A TOOLING HOLE) IN PULLEY BRACKET P/N:6960236-17. THIS CAUSED AN INTERFERENCE AND WEAR IN THE PULLEY BRACKET, AND FLAT AREAS TO THE CABLE. CABLE AND SDR NOB2007F00000Spring · obstructedNLG WOULD NOT EXTEND WHILE ON APPROACH. AC RETURNED & THROUGH G-LOAD MANUEVERS, MANAGED TO GET NLG TO EXTEND PRIOR TO LANDING. PROBLEM WAS DETERMINED TO BE INTERFERENCE BETWEEN NLG CENTERING SPRING ROD END ATTACHMENT CLEVIS BOLT HEAD AND REAR TORQUE TUBE FOSDR CA060502008Battery · leaking(CAN) ELT BATTERIES LEAKED. (TC NR 20060502008)SDR AU510002146Hinge · corrodedRUDDER HINGE BRACKET CORRODED.SDR 2005FA0000108Shaft · out of roundUPON INSTALLING A SHAFT INTO A ROCKER WITH INADEQUATE TOLERANCE LIMITS, NOTED BINDING IN THREE CLOCK POSITIONS. WITH PRUSSION BLUE, FOUND THAT THE SHAFT IS FORMED IN AN ELIPTICAL OR, MODIFIED TRI-ANGULAR SHAPE WITH REDUCED WEAR SURFACE AREA DUE TO INCONSISTANTSDR 2005FA0000484Shaft · out of roundUPON INSTALLING A SHAFT INTO A ROCKER WITH INADEQUATE TOLERANCE LIMITS, NOTED BINDING IN 3 O`CLOCK POSITIONS. WITH PRUSSION BLUE FOUND SHAFT IS FORMED IN ELIPTICAL OR, MODIFIED TRIANGULAR SHAPE WITH REDUCED WEAR SURFACE AREA DUE TO INCONSISTANT DIA OF SHAFT. SDR CA040901001Tube · out of tolerance(CAN) TUBE PURCHASED NEW. INSTALLED NEW. TEE SHOOTING AT VARIOUS REPAIR STATIONS DISCOVER CIRCLIP GROOVE TOO SMALL TO ACCOMODATE FULL CLIP SEATING. (GROOVE UNDERSIZED)NEW TUBE PURCHASED AND REPLACED. NO FAULT TO DATE. INITIAL RECURRING FAULTS INC LUDED, LOSS SDR AUS20040204Tube · worn(AUS) NOSE LANDING GEAR EXTENSION HYDRAULIC PIPE WORN THROUGH BY CONTACT WITH THE NLG BRAKE FLUID COVER ASSEMBLY. LOSS OF HYDRAULIC FLUID.SDR CA030729020Door · cracked(CAN) CRACKS ON THE MAIN LANDING GEAR DOOR FLANGE. BOTH LT AND RT DOOR. DOOR IS FIBERGLASS COMPOSITE STRUCTURE. MAIN LANDING GEAR DOOR LT PN 67090-10 MAIN LANDING GEAR DOOR RT PN 67090-11.SDR AUS20030413Fitting · fractured(AUS) LEFT ENGINE FUEL LINE FITTING FAILED. FUEL LEAK.SDR AUS20030371Spar Cap · corroded(AUS) RH STABILATOR LOWER SPAR CAP CORRODED.SDR CA030107018Line · corroded(CAN) DURING A GROUND RUN FOR CALIBRATION OF AN UNRELATED SYSTEM THE ENGINEER NOTICED A STRONG FUEL SMELL IN THE CABIN. THE SOURCE WAS FOUND TO BE A CORRODED HEATER FUEL LINE AT APPROXIMATELY FS 165. THE CARPET AHEAD OF PASSENGER SEAT NR 6 WAS SOAKED WITH FUELSDR AUS20020713Cable · separated(AUS) FORWARD LH STABILATOR TRIM CABLE DISCONNECTED FROM TRIM WHEEL.BALL END OF CABLE HAD COME OUT OF THE SOCKET ON THE SIDE OF THE WHEEL.SDR AUS20011341Bolt · broken(AUS) STABILISER ATTACHMENT FITTING BOLTS BENT (2OFF) AND BROKEN(2OFF). INVESTIGATION FOUND THAT THE BOLTS WERE THE INCORRECT TYPE. THE PART NUMBER OF THE INCORRECT BOLTS WAS PNO NAS425-3-7.UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR.SDR AUS20011183Housing · cracked(AUS) LH AND RH ENGINE TURBOCHARGER TURBINE HOUSINGS CRACKED. FOUND DURING INSPECTION IAW AD/TURBO/1. LH ENGINE - CONTINENTAL TSIO-360-E - SERIAL NUMBER 307156 TSO 338.6 HOURS - TSLSV 119.6 HOURS RH ENGINE - CONTINENTAL LTSIO-360-E - SERIAL NUMBER 306161TSO 33SDR AU000624Stud · wrong part(AUS) BOTH PROPELLERS COULD NOT BE FITTED CORRECTLY DURING INSTALLATION TO RECENTLY OVERHAULED ENGINES. SUBSEQUENT INVESTIGATION FOUND THE ATTACHING STUDS WERE TOO LONG (-4 STUDS HAD BEEN FITTED INLIEU OF -3 STUDS). (X)SDR 20000809SH004Magneto · failedTEST RUN SHOWED MAGNETO TO BE DEAD. REMOVED AND DISASSEMBLED MAGNETO. FOUND WIPER TAB FOR DISTRIBUTOR GEAR TO BE SHEARED OFF OF GEAR. (X)SDR AU000330Crankcase · cracked(AUS) CRANKCASE CRACKED IN NUMEROUS PLACES. CRANKCASE HAD BEENPREVIOUSLY WELD REPAIRED.SDR AU991037Stall Warning · malfunctioned(AUS) STALL WARNING SYSTEM FAULTY. SYSTEM WORKS PERFECTLY ON THE GROUND BUT FAILS TO OPERATE IN THE AIR. THE SYSTEM HAS BEEN THOROUGHLY CHECKED WITH NUMEROUS COMPONENT CHANGES TO NO AVAIL.SDR 2000ZZZX163Fuel Pump · brokenAIRCRAFT WAS EN ROUTE FROM OWA TO HTO, CRUISE AT 4,500 MSL. EXPERIENCED ENGINE AND FUEL FLOW FLUCTUATIONS, THEN COMPLETE LOSS OF POWER. WAS CLOSE TO WST, SECURED LEFT ENGINE AND LANDED. REEVES AIR INSPECTED AND FOUND LEFT ENGINE DRIVEN FUEL PUMP INOPERABLE.SDR AU990854Co2 Detector · faulty(AUS) CARBON DIOXIDE DETECTOR FAULTY.SDR AU990836Liner · unserviceable(AUS) CABIN HEATER COMBUSTION LINER FAILED. FOUND DURING INSPECTION IAW AD/AIRCON/9 AMDT5.SDR CA991231062Cotter Pin · broken(CAN) COTTER PIN FOUND IN OIL SCREEN AT 100HR INSP.SDR CA991231063Crankshaft · cracked(CAN) TWO CRACKS FOUND BY NDI SHOP, CRANK REJECTED.SDR AU980280Crankcase · cracked(AUS) ENGINE CRANKCASE RT HALF CRACKED IN NR 4 MAIN BEARING TUNNEL AND LT HALF CRACKED IN NR 2 AND NR 3 MAIN BEARING TUNNELS. CRANKSHAFT CRACKED ON NR 4 MAIN BEARING. CRACK LENGTH APPROXIMATELY 50.8MM (2 INCHES).SDR CA980302002Cylinder · separated(CAN) THE TOP OF THE CYLINDER CONTAINING THE VALVES AND THE ROCKER ARMS SEPARATED FROM THE CYLINDER.SDR CA971016002Piston Ring · broken(CAN) DURING CYLINDER REMOVAL TO CORRECT AN OIL CONSUMPTION PROBLEM, IT WAS FOUND THAT PISTON RING (P/N 684042) WAS BROKEN. IT APPEARS THERE WAS A CASTING PROBLEM DURING MANUFACTURER.SDR AU970799Cylinder · distorted(AUS) NO6 CYLINDER EXHAUST FLANGE DISTORTED - 2MM (0.078IN) GAP ON FORWARD SIDE - FURTHER INVESTIGATION FOUND NO2 AND NO4 CYLINDERS WITH APPROXIMATELY 1MM (0.039IN) GAPS - HEAT DAMAGE TO ENGINE COWLS FROM LEAKING EXHAUST GASSES - NEW GASKETS HAD BEEN FITTED APSDR AU970915Bearing · bindiing(AUS) LH ENGINE MIXTURE CONTROL ROD END BEARING AND CONTROL ARM BINDING ON FCUSDR AU960808Exhaust Valve · failed(AUS) LH ENGINE NO5 CYLINDER EXHAUST VALVE FAILED - SUSPECT CAUSED BY EXCESSIVE LEANING OF ENGINESDR 96ZZZX938Line · brokeFUEL LINE FROM FLOW DIVIDER TO NR 6 NOZZLE BROKE AT B-NUT NOZZLE AND SPRAYED RAW FUEL ON ENGINE. ENGINE ROUGH, BUT NOT SHUT DOWN AND LANDED OK WITH NO FIRE. VERY LUCKY!SDR CA951218018Fuel Pump · faulty(CAN)DURING A TRAINING FLIGHT,AT 5,000 FEET,THE #2 ENGINE HAD A LOSS OF POWER & THE LOWERING OF PRESSURE ON THE FUEL FLOW INDICATOR.THE #2 ENGINE WAS SHUTDOWN & THE AIRCRAFT LANDED.AFTER ARRIVAL THE #2 ENG INE WAS RUN UP,THREE TIMES IT FAILED TO EXCEED 2,000 RSDR BIER950010Adapter Shaft · shearedTACH INDICATED 0 RPM BUT ENGINE RAN NORM. FOUND TACH DRIVE ADAPTER SHEARED AT ATTACH NUT. REMOVED AND REPL WITH NEW.SDR 96ZZZX4786Crankcase · crackedDURING TROUBLESHOOTING TO DETERMINE ORIGIN OF AN OIL LEAK, FOUND CASE CRACKED ON BOTH VALVES AT NR 3 BEARING WEB. UPON TEAR DOWN, CASE HALVES WERE REJECTED DUE TO FAILING HARDNESS TEST. CRACKS WERE IN AREA OF A PREVIOUS REPAIR. CAUSE OF FAILURE UNKNOWN.
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