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.

SDR 2015FA0000298Pump · low pressureTHE ENGINE DRIVEN FUEL PUMP HAS LOW FUEL FLOW.May 17, 2015 · Cirrus SR20 · Engine Fuel PumpSDR 2015FA0000304Warning Light · illuminated(B9573) LOW FUEL FLOW WHILE TAKING OFF.Apr 16, 2015 · Cirrus SR20 · Engine Fuel DistributionSDR 2015FA0000303Warning Light · illuminated(B9583) LOW FUEL FLOW ON THE GROUND.Apr 11, 2015 · Cirrus SR20 · Engine Fuel DistributionSDR 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 OFApr 10, 2015 · N587PU · Cirrus SR20 · Engine Fuel PumpSDR 2015FA0000136Pump · leaking(B-9571) LOW FUEL FLOW WAS INDICATED DURING TAKEOFF.Apr 9, 2015 · Cirrus SR20 · Engine Fuel PumpSDR 2015FA0000139Pump · leaking(B-9736) FIELD MECHANIC FOUND FUEL LEAKAGE.Apr 7, 2015 · Cirrus SR20 · Engine Fuel PumpSDR 2015FA0000138Pump · leaking(B-9578) LOW FUEL FLOW WAS INDICATED DURING TAKING OFF.Apr 6, 2015 · Cirrus SR20 · Engine Fuel PumpSDR 2015FA0000135Pump · leaking(B-9733) LOW FUEL FLOW WAS INDICATED DURING TAKING OFF.Mar 25, 2015 · Cirrus SR20 · Engine Fuel PumpSDR 2015FA0000097Pump · malfunctionedENGINE RPM DECREASE WHEN PUMP IN BOOST. PREFLIGHT RUN UP. GROWING NOISE FROM PUMP.Mar 19, 2015 · Cirrus SR20 · Fuel Boost PumpSDR 2015FA0000134Pump · leaking(B-9571) FIELD MECHANIC FOUND FUEL LEAKAGE ON 19TH MARCH.Mar 19, 2015 · Cirrus SR20 · Engine Fuel PumpSDR 2015FA0000133Pump · leaking(B-9739) LOW FUEL FLOW ABOUT 13.3 G/H WAS INDICATED DURING FULL THROTTLE.Feb 6, 2015 · Cirrus SR20 · Engine Fuel PumpSDR 2015FA0000051Magneto · contaminatedA STONE WAS FOUND IN THE MAGNETO HOUSING DURING ITS FIRST 500 HOURS INSPECTION.Jan 28, 2015 · Cirrus SR20 · Magneto/DistributorSDR 2015FA0000029Tube · crackedENGINE MAKES A POPPING NOISE WHEN PULLING THROTTLE BACK TO IDLE. FOUND CRACKED INTAKE TUBE.Jan 26, 2015 · Cirrus SR20 · Engine Air Intake SystemSDR 2015FA0000132Pump · leaking(B-9733) LOW FUEL FLOW, ABOUT 15.3 G/H, WAS INDICATED DURING FULL THROTTLE.Jan 13, 2015 · Cirrus SR20 · Engine Fuel PumpSDR 2015FA0000131Pump · leaking(B-9731) LOW FUEL FLOW WAS INDICATED DURING FULL THROTTLE.Jan 6, 2015 · Cirrus SR20 · Engine Fuel PumpSDR 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.Jan 3, 2015 · Cirrus SR20 · Engine Fuel PumpSDR 2015FA0000001Pump · leaking(B9737) FUEL FLOW SUDDENLY DROPPED TO 12.3 G/H DURING TAKEOFF, AND THE ENGINE RUN SMOOTHLY.Dec 13, 2014 · Cirrus SR20 · Fuel Control/Reciprocating EnginesSDR 2014FA0000595Pump · leakingWHEN DOING FUEL SYSTEM SEAL TEST, FOUND FUEL LEAKING FROM THE MIXTURE CONTROL SHAFT OF THE ENGINE DRIVEN FUEL PUMP.Oct 10, 2014 · Cirrus SR20 · Engine Fuel PumpSDR 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 Sep 29, 2014 · Cirrus SR20 · Engine Fuel PumpSDR 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 PSep 24, 2014 · Cirrus SR20 · Engine Fuel PumpSDR 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 FUESep 23, 2014 · Cirrus SR20 · Engine Fuel PumpSDR 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 ANDSep 17, 2014 · N581PU · Cirrus SR20 · Engine Fuel PumpSDR 2014FA0000457Pump · failedENGINE FUEL PUMP FAILED.Aug 4, 2014 · N311LS · Cirrus SR20 · Fuel Boost PumpSDR 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.Jul 16, 2014 · N487DA · Cirrus SR20 · Reciprocating Engine Power SectionSDR 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.Jul 14, 2014 · N486JG · Cirrus SR20 · Engine RPM Indicating SystemSDR 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.Jun 30, 2014 · N311LS · Cirrus SR20 · Engine Fuel PumpSDR 2014FA0000282Magneto · faultyOBVIOUS VIBRATION HAPPENED AT TAKEOFF, THE PLANE LANDED TO INSPECT. LOOSENED BUSHING IN THE DISTRIBUTOR WAS FOUND AFTER DISASSEMBLING THE MAGNETO.Apr 28, 2014 · Cirrus SR20 · Magneto/DistributorSDR 2014FA0000283Magneto · faultyOBVIOUS VIBRATION HAPPENED DURING LEVER FLIGHT, THE PLANE LANDED TO INSPECT. LOOSENED BUSHING IN THE DISTRIBUTOR WAS FOUND AFTER DISASSEMBLING THE MAGNETO.Apr 28, 2014 · Cirrus SR20 · Magneto/DistributorSDR 2014FA0000284Magneto · faultyOIL LEAKING IN THE MAGNETO HOUSING CAUSED ENGINE VIBRATION.Apr 28, 2014 · Cirrus SR20 · Magneto/DistributorSDR 2014FA0000285Magneto · faultyOIL LEAKING IN THE MAGNETO HOUSING CAUSED ENGINE VIBRATION.Apr 28, 2014 · Cirrus SR20 · Magneto/DistributorSDR 2014FA0000259Bracket · crackedNR 1 ALTERNATOR BRACKET CRACK FOUND DURING INSPECTION AT THE ALTERNATOR BRACKET MOUNTING HOLE.Apr 18, 2014 · Cirrus SR20 · DC Generator-AlternatorSDR 2014FA0000281Magneto · faultyOBVIOUS VIBRATION HAPPENED AT TAKEOFF, THE PLANE LANDED TO INSPECT. LOOSENED BUSHING IN THE DISTRIBUTOR WAS FOUND AFTER DISASSEMBLING THE MAGNETO.Mar 31, 2014 · Cirrus SR20 · Magneto/DistributorSDR 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/DMar 24, 2014 · Cirrus SR20 · Electrical Power SystemSDR 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 BACKPLDec 17, 2013 · Cirrus SR20 · Propeller Spinner SectionSDR 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.Dec 4, 2013 · N263HB · Cirrus SR20 · Reciprocating Engine Power SectionSDR 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.Dec 4, 2013 · N83CD · Cirrus SR20 · Reciprocating Engine Power SectionSDR 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 CONTRSep 11, 2013 · N156KT · Cirrus SR20 · Engine Fuel PumpSDR 2013FA0000434Bracket · crackedALTERNATOR BRACKET HAS CRACKING FOUND AROUND THE UPPER-AFT MOUNTING BOLT.Aug 8, 2013 · Cirrus SR20 · Engine Starting SystemSDR 2013FA0000435Bracket · crackedALTERNATOR BRACKET HAS CRACKS FORMED AROUND THE UPPER AFT BOLT AS SEEN FROM ABOVE.Aug 8, 2013 · Cirrus SR20 · Engine Starting SystemSDR 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 PEMay 20, 2013 · N851ST · Cirrus SR20 · Magneto/DistributorSDR 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 CRMar 14, 2013 · N36PL · Cirrus SR20 · Ignition System WiringSDR 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.Nov 7, 2012 · N156KT · Cirrus SR20 · Ignition System WiringSDR 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.Oct 30, 2012 · Cirrus SR20 · Trailing Edge FlapsSDR 2012FA0000709Pump · out of toleranceENGINE DRIVEN MECHANICAL FUEL PUMP WOULD NOT DELIVER ADEQUATE FUEL FLOW AFTER ADJUSTMENT.Sep 29, 2012 · N610DA · Cirrus SR20 · Engine Fuel PumpSDR 2012FA0000649Bracket · crackedCRACK DISCOVERED IN ALTERNATOR MOUNTING BRACKET, PN 657046. THIRD OCCURANCE OF THIS PROBLEM.Sep 26, 2012 · Cirrus SR20 · Electrical Power SystemSDR 2012FA0000650Mount Bracket · crackedCRACK DISCOVERED IN ALTERNATOR MOUNTING BRACKET, PN 657046. THIRD OCCURANCE OF THIS PROBLEM. REF 2012FA0000649.Sep 26, 2012 · N93ER · Amrgen AG5B · DC Generator-AlternatorSDR 2012FA0000720Magneto · malfunctionedMAGNETO MISFIRES DURING MAGNETO CHECK.Sep 1, 2012 · N476DA · Cirrus SR20 · Magneto/DistributorSDR 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 COWLINGAug 24, 2012 · N156CS · Cirrus SR20 · Engine StarterSDR 2012FA0000725Magneto · malfunctionedENGINE MISFIRES WHEN CHECKING LEFT MAGNETO.Aug 18, 2012 · N610DA · Cirrus SR20 · Magneto/DistributorSDR 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.Aug 16, 2012 · N478DA · Cirrus SR20 · Engine Fuel Pump
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