Continental IO-360-ES
Service difficulty reports · 176
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 = 'IO360ES' 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 = 'IO360ES' 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 2015FA0000298Pump · low pressureTHE ENGINE DRIVEN FUEL PUMP HAS LOW FUEL FLOW.SDR 2015FA0000304Warning Light · illuminated(B9573) LOW FUEL FLOW WHILE TAKING OFF.SDR 2015FA0000303Warning Light · illuminated(B9583) LOW FUEL FLOW ON THE GROUND.SDR 2015FA0000568Pump · low pressureDURING A ACFT PROGRESSIVE INSPECTION, PROGRAM 50 HR INSPECTION DISCOVERED ENGINE FUEL FLOW TO BE LOW OUT OF LIMITS. IN THIS CASE WE WERE ABLE TO ADJUST THE FUEL FLOW TO WITHIN LIMITS IAW CMI SID97-3F. DURING FLIGHT CHECK IAW SID97-3, FUEL FLOW WAS LOW OUT OFSDR 2015FA0000136Pump · leaking(B-9571) LOW FUEL FLOW WAS INDICATED DURING TAKEOFF.SDR 2015FA0000139Pump · leaking(B-9736) FIELD MECHANIC FOUND FUEL LEAKAGE.SDR 2015FA0000138Pump · leaking(B-9578) LOW FUEL FLOW WAS INDICATED DURING TAKING OFF.SDR 2015FA0000135Pump · leaking(B-9733) LOW FUEL FLOW WAS INDICATED DURING TAKING OFF.SDR 2015FA0000097Pump · malfunctionedENGINE RPM DECREASE WHEN PUMP IN BOOST. PREFLIGHT RUN UP. GROWING NOISE FROM PUMP.SDR 2015FA0000134Pump · leaking(B-9571) FIELD MECHANIC FOUND FUEL LEAKAGE ON 19TH MARCH.SDR 2015FA0000133Pump · leaking(B-9739) LOW FUEL FLOW ABOUT 13.3 G/H WAS INDICATED DURING FULL THROTTLE.SDR 2015FA0000051Magneto · contaminatedA STONE WAS FOUND IN THE MAGNETO HOUSING DURING ITS FIRST 500 HOURS INSPECTION.SDR 2015FA0000029Tube · crackedENGINE MAKES A POPPING NOISE WHEN PULLING THROTTLE BACK TO IDLE. FOUND CRACKED INTAKE TUBE.SDR 2015FA0000132Pump · leaking(B-9733) LOW FUEL FLOW, ABOUT 15.3 G/H, WAS INDICATED DURING FULL THROTTLE.SDR 2015FA0000131Pump · leaking(B-9731) LOW FUEL FLOW WAS INDICATED DURING FULL THROTTLE.SDR 2015FA0000127Pump · leaking(B-9749) WHEN CHECKED, THE FUNCTION BOOST AND PRIME OF THE ENGINE DRIVEN FUEL PUMP, THERE WAS A LITTLE FUEL LEAKING FROM MIXTURE SEAT.SDR 2015FA0000001Pump · leaking(B9737) FUEL FLOW SUDDENLY DROPPED TO 12.3 G/H DURING TAKEOFF, AND THE ENGINE RUN SMOOTHLY.SDR 2014FA0000595Pump · leakingWHEN DOING FUEL SYSTEM SEAL TEST, FOUND FUEL LEAKING FROM THE MIXTURE CONTROL SHAFT OF THE ENGINE DRIVEN FUEL PUMP.SDR 2014FA0000580Pump · leakingGROUND SEAL TEST TO THE FUEL SYSTEM, FOUND FUEL LEAKING FROM THE VENT TUBE OF ENGINE DRIVEN FUEL PUMP. ACCORDING TO THE STRUCTURE AND FUNCTION OF THE PUMP, IT'S ONLY BROKEN SEAL DIAPHRAGM BETWEEN THE LOW PRESSURE SCREW AND THE PUMP BODY CAN CAUSE FUEL LEAKING SDR 2014FA0000578Pump · leakingFUEL LEAKING PROBLEM HAPPENED IN THE SR20 FLEET, SO DO SAME FAULT INSPECTION TO ALL THE SR20 AIRPLANES, THEN FOUND THIS ONE HAD THE FUEL LEAKING FAULT ON THE ENGINE DRIVEN FUEL PUMP. IT'S THE SAME LEAKING LOCATION ON THE MIXTURE CONTROL SHAFT TO OTHER FAULTY PSDR 2014FA0000576Pump · leakingMECHANIC FOUND FUEL LEAKAGE BLUE COLOR ON THE BOTTOM OF THE ENGINE COWLING DURING IN-FLIGHT INSPECTION. THEN EXAMINED AND FOUND THE LEAKAGE WAS FROM THE MIXTURE CONTROL ARM OF THE ENGINE DRIVEN PUMP. TURNED ON THE BOOST PUMP TO MAKE FUEL PRESSURE, A LOT OF FUESDR 2015FA0000564Pump · low pressurePILOTS REPORTED LOW FUEL FLOW ON TAKEOFF OF 13.5 GALLONS PER HOUR. WE HAVE ESTABLISHED AN OPERATIONAL MINIMUM FUEL FLOW OF 16.0 GALLONS PER HOUR DUE TO OUR EXPERIENCE WITH THESE ENGINE DRIVEN FUEL PUMP ANEROID FAILURES. ATTEMPTED TO ADJUST PUMP IAW SID97-3 ANDSDR 2014FA0000457Pump · failedENGINE FUEL PUMP FAILED.SDR 2014FA0000433Gear · brokenDURING 100 HR INSPECTION, A GEAR TOOTH WAS FOUND IN OIL SUMP. AFTER FURTHER INSPECTION IT WAS FOUND TO BE A TOOTH FROM THE TIMING GEAR ON THE CRANKSHAFT.SDR 2014FA0000429Tach Generator · failedTHE ENGINE TACHOMETER WOULD NOT REGISTER BELOW 1000 RPM. REPLACED THE TACH GENERATOR AND DISCOVERED THE KEYWAY ON THE SHAFT HAD WORN OFF. LOG BOOK RESEARCH SHOWED THAT THE SAME PROBLEM OCCURRED IN 2007 AT TTAF 253.5.SDR 2014FA0000413Bellows · mismanufacturedTLEP TELLS US ANEROID BELLOWS IN FUEL PUMPS HAVE MFG DEFECT. ALL AFFECTED UNITS HAVE BEEN IDENTIFIED AND REMOVED FROM INVENTORY. THIS SCENARIO HAS RESULTED IN MULTIPLE FUEL PUMP CHANGES MANDATING THIS SUBMISSION.SDR 2014FA0000282Magneto · faultyOBVIOUS VIBRATION HAPPENED AT TAKEOFF, THE PLANE LANDED TO INSPECT. LOOSENED BUSHING IN THE DISTRIBUTOR WAS FOUND AFTER DISASSEMBLING THE MAGNETO.SDR 2014FA0000283Magneto · faultyOBVIOUS VIBRATION HAPPENED DURING LEVER FLIGHT, THE PLANE LANDED TO INSPECT. LOOSENED BUSHING IN THE DISTRIBUTOR WAS FOUND AFTER DISASSEMBLING THE MAGNETO.SDR 2014FA0000284Magneto · faultyOIL LEAKING IN THE MAGNETO HOUSING CAUSED ENGINE VIBRATION.SDR 2014FA0000285Magneto · faultyOIL LEAKING IN THE MAGNETO HOUSING CAUSED ENGINE VIBRATION.SDR 2014FA0000259Bracket · crackedNR 1 ALTERNATOR BRACKET CRACK FOUND DURING INSPECTION AT THE ALTERNATOR BRACKET MOUNTING HOLE.SDR 2014FA0000281Magneto · faultyOBVIOUS VIBRATION HAPPENED AT TAKEOFF, THE PLANE LANDED TO INSPECT. LOOSENED BUSHING IN THE DISTRIBUTOR WAS FOUND AFTER DISASSEMBLING THE MAGNETO.SDR CA140401019Bracket · cracked(CAN) DURING THE ANNUAL INSPECTION OF THIS ACFT, THE FORWARD ALTERNATOR BRACKET WAS FOUND CRACKED AFTER ONLY 240.8HRS, 2 YEARS SINCE ITS REPLACEMENT IN MARCH 2012. THE BRACKET IS AN OEM REPLACEMENT. THE ORIGINAL BRACKET WAS ALSO REPLACED DUE TO SAME FAILURE/DSDR CA131219014Plate · cracked(CAN) DURING HANGAR MOVEMENT THE SPINNER WAS NOTICED TO BE LOOSE. WHEN THE SPINNER WAS REMOVED, THE INSIDE OF SPINNER WAS ALL BLACK FROM CHAFING AND THE BULKHEAD WAS CRACKED. THE SPINNER BACKPLATE WAS SEVERELY CRACK FROM ALL 4 MOUNTING HOLES. WHEN THE BACKPLSDR 5CSR2013FA0000777Case · crackedOIL ON WINDSCREEN. ON CLEANING ENGINE, A CRACK WAS FOUND ABOUT 4 INCHES IN LENGTH FROM THE ALTERNATOR BRACKET ACROSS THE RT UPPER SECTION OF THE CASE.SDR 5CSR2013FA0000778Case · crackedDURING AN OIL CHANGE, ENGINE WAS NOTED TO HAVE LARGE AMOUNT OF OIL IN THE COWLING AND ON THE ENGINE. AFTER CLEANING ENGINE, A CRACK WAS FOUND ABOUT 3 INCHES IN LENGTH FROM THE ALTERNATOR BRACKET ACROSS THE RT UPPER SECTION OF THE CASE.SDR 2013FA0000566Pump · malfunctionedDURING ENGINE OPERATION, THE MIXTURE CONTROL STOP PIN HAD BECOME LOOSE AND VIBRTED OUT PARTIALLY, LOCKING THE MIXTURE IN THE FULL RICH POSITION. IT IS SUSPECTED THAT DUE TO HEAVY USE AS A TRAINING ACFT WITH REPEATED STOP TO STOP OPERATION OF THE MIXTURE CONTRSDR 2013FA0000434Bracket · crackedALTERNATOR BRACKET HAS CRACKING FOUND AROUND THE UPPER-AFT MOUNTING BOLT.SDR 2013FA0000435Bracket · crackedALTERNATOR BRACKET HAS CRACKS FORMED AROUND THE UPPER AFT BOLT AS SEEN FROM ABOVE.SDR 2013FA0000291Coil · failedDURING GROUND RUN-UP PRIOR TO TAKEOFF, AS PILOT CYCLED TO RT MAGENTO, ENGINE ATTEMPTED TO CUT-OUT BUT PILOT WAS ABLE TO KEEP RUNNING BY SWITCHING MAGNETO SWITCH BACK TO "BOTH". FLIGHT CREW RETURNED TO RAMP AND SQUAWKED ACFT FOR DEAD MAGNETO ON RT SIDE. MX PESDR 2013FA0000197Wire · brokenDURING TAXI IN, ENGINE WAS VIBRATING AND MIS-FIRING AT OR BELOW 1000 RPM. MX PERSONNEL DUPLICATED PROBLEM BY PLACING MAGNETO SWITCH ON RT MAG ONLY. RT MAGNETO WAS REMOVED TO DISCOVER COIL PRIMARY LEAD TO POINTS HAD BROKEN OFF. COIL LEAD WIRE HAD NOT BEEN CRSDR 2012FA0000770Wire Harness · wornMORE THAN 10 AREAS OF THE IGNITION WIRE HARNESS HAD WORN THROUGH THE SHIELDING. TWO WIRES WOULD NOT PASS HIGH TENSION TEST. THIS IS THE THIRD ACFT WITH THIS CONDITION BUT IT IS THE WORST.SDR CA130402004Hinge · corroded(CAN) INSPECTION OF FLAP HINGES FOUND CORROSION, EXFOILATION AND INTERGRANULAR CORROSION ON UPPER PORTION OF HINGES. REPLACE ALL FLAP HINGES, PIN 14572-008, INBD RT PIN 14571-007, MIDDLE LT AND RT PIN 14572-004 OTBD LT AND RT PIN 14573-004.SDR 2012FA0000709Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WOULD NOT DELIVER ADEQUATE FUEL FLOW AFTER ADJUSTMENT.SDR 2012FA0000649Bracket · crackedCRACK DISCOVERED IN ALTERNATOR MOUNTING BRACKET, PN 657046. THIRD OCCURANCE OF THIS PROBLEM.SDR 2012FA0000650Mount Bracket · crackedCRACK DISCOVERED IN ALTERNATOR MOUNTING BRACKET, PN 657046. THIRD OCCURANCE OF THIS PROBLEM. REF 2012FA0000649.SDR 2012FA0000720Magneto · malfunctionedMAGNETO MISFIRES DURING MAGNETO CHECK.SDR 2012FA0000603Starter · burnedAFTER ENGINE START THE MAP, ENGINE PERCENT POWER AND FUEL FLOW INDICATIONS BECAME INOPERATIVE. ACFT WAS NOT FLOWN. FLIGHT CREW SQUAWKED PROBLEM AND BROUGHT ACFT AND TIN TO MX. GROUND RUN-UP PERFORMED AND AMT WAS ABLE TO DUPLICATE PROBLEM. ACFT ENGINE COWLINGSDR 2012FA0000725Magneto · malfunctionedENGINE MISFIRES WHEN CHECKING LEFT MAGNETO.SDR 2012FA0000707Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WILL NOT OUTPUT HIGHER THAN 13 GPH AFTER ADJUSTMENT. OUTPUT SHOULD BE IN THE 17 - 18 GPH RANGE.
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