# Service difficulty reports: Continental IO-360-ES A list on [Continental IO-360-ES](https://openairdocs.org/engine/continental-io-360-es.md). Newest first. General aviation reporting is voluntary. Page 1 of 4 · 176 reports - [SDR 2024FA0000534](https://openairdocs.org/sdr/2024FA0000534.md): Drive Coupling · broken · Jul 26, 2024 · N2117 · Cirrus SR20 · DC Generator-Alternator > GEAR PORTION OF COUPLER SLIPS INSIDE METAL/RUBBER HOUSING, CAUSING ALTERNATOR #2 TO REMAIN OFFLINE. A SECOND ALTERNATOR EXISTS WITHIN THE SYSTEM, SO NO INITIAL SAFETY OF FLIGHT ISSUES WITH LOSS OF POWER IF LANDING IS ACCOMPLISHED IN A TIMELY MANNER. THIS IS TH - [SDR 2024FA0000147](https://openairdocs.org/sdr/2024FA0000147.md): Magneto · misoverhauled · Feb 5, 2024 · N290CD · Cirrus SR20 · Magneto/Distributor > REBUILT T WAS DETERMINED TO BE FAULTY OUT OF THE BOX BY THE SHOP TECHNICIAN PERFORMING INSTALL OF MAGNETO TO THE AIRCRAFT. TECHNICIAN TESTED AND VERIFIED REBUILT MAGNETO WAS FAULTY OUT OF THE BOX. TECHNICIAN REMOVED FAULTY OUT OF THE BOX MAGNETO FROM THE AIRC - [SDR 2023FA0000241](https://openairdocs.org/sdr/2023FA0000241.md): Fuel Divider · inoperative · May 1, 2023 · N163CD · Cirrus SR20 · Fuel Divider > PILOT COMPLETED A SATISFACTORY ENGINE RUN. CLIMBING OUT, ENGINE STARTS TO RUN ROUGH. PILOT NOTICES FUEL DROPLETS ON WINDSCREEN. ENGINE QUITS WHILE THROTTLE IS FULL POWER AND MIXTURE IS FULL RICH. PILOT CIRCLES BACK, DECLARES EMERGENCY AND SAFELY LANDS AIRCRAFT - [SDR 2021FA0000269](https://openairdocs.org/sdr/2021FA0000269.md): Exhaust Rocker · sheared · Sep 30, 2021 · Cirrus SR20 · Engine (Reciprocating) > AIRCRAFT LANDED AFTER NOTICEABLE POWER LOSS. DURING DETAILED VISUAL INSPECTION, DISCOVERED #3 CYLINDER EXHAUST ROCKER ATTACH STUDS SHEARED AT CYLINDER. ROCKER WAS FREE-FLOATING IN ROCKER COVER. *SERIAL NUMBER NOT FOUND IN AIRCRAFT INQUIRY - [SDR 2019FA0000399](https://openairdocs.org/sdr/2019FA0000399.md): Bracket · worn · Dec 9, 2019 · N2075T · Cirrus SR20 · Flight Control System > RUDDER AILERON INTERCONNECT STOPPED FUNCTIONING. DISCOVERED BRACKETS WORN THROUGH. NO CHAFING ON CONTROL CABLES FORTUNATELY. PART NO LONGER MANUFACTURED. - [SDR 2019FA0000096](https://openairdocs.org/sdr/2019FA0000096.md): Spark Plug · damaged · Mar 4, 2019 · N588PU · Cirrus SR20 · Spark Plug/Igniter > AIRCRAFT RETURNED TO AIRPORT SHORTLY AFTER TAKEOFF CLIMB DUE TO SMOKE AND FUMES IN COCKPIT. PILOT ALSO RECEIVED HIGH CHT AND HIGH EGT INDICATIONS FROM #1 CYLINDER. PILOT REDUCED POWER, LOWERED NOSE AND PERFORMED UNEVENTFUL RETURN TO AND LANDING AT DEPARTURE AI - [SDR O6WR201812130001](https://openairdocs.org/sdr/O6WR201812130001.md): Keyway · worn · Dec 12, 2018 · N1218P · Cirrus SR20 · Engine RPM Indicating System > KEY ON DRIVE SHAFT FROM ENGINE TO TACHOMETER GENERATOR WORE AWAY CAUSING LOW/NO RPM INDICATION. FAILURE AFTER ONLY 106HRS MAY INDICATE POSSIBLE MANUFACTURE DEFECT - [SDR 2018FA0000117](https://openairdocs.org/sdr/2018FA0000117.md): Hinge Bracket · corroded · Mar 23, 2018 · N579W · Cirrus SR20 · Flight Control System > PROBLEM AREA BY VISUAL INSPECTION - RIGHT AND LEFT FLAP HINGE BRACKET SEVERE CORROSION AND PRONE TO CRACKS LEADING UP TO THE BOLT HOLES THAT ATTACH THE BRACKET TO THE AIR FRAME OR AT THE FLAP MOUNTING HOLES IF CORROSION PROGRESSES AND NOT DETECTED AND CAN LEAD - [SDR 2017FA0000049](https://openairdocs.org/sdr/2017FA0000049.md): Probe · erratic · Feb 8, 2017 · N159PG · Cirrus SR20 · Engine Oil System Wiring > PERFORMED INITIAL ENGINE RUNUP, BECAUSE HIGH NR 2 CHT WAS REPORTED. AFTER ENGINE WAS WARMED UP DID FULL POWER STAIC RUN UP, NO ABNORMAL TEMPS WERE NOTED. BORESCOPED CYLINDER, NO DISCREPANCIES WERE NOTED. VISUALLY INSPECTED EXTERIOR OF CYLINDER FOR CRACKS OR LO - [SDR CG9S2016FA0000409](https://openairdocs.org/sdr/CG9S2016FA0000409.md): Pump · low pressure · Aug 30, 2016 · N580PU · Cirrus SR20 · Engine Fuel Pump > DURING A MAINTENANCE CHECK FLIGHT, THE AIRCRAFT LOST ENGINE POWER APPROXIMATELY 2-3 MILES FROM AIRPORT ON APPROACH. ACFT WAS ABLE TO LAND UNEVENTFULLY ON ANOTHER RUNWAY AT THE SAME AIRPORT. PILOT STATED HE WAS APPROACHING AIRPORT FROM WEST AND WAS DIRECTED T - [SDR 2016FA0000407](https://openairdocs.org/sdr/2016FA0000407.md): Pump · leaking · Aug 28, 2016 · Cirrus SR20 · Fuel Boost Pump > LEAKAGE IN THE ELECTRIC FUEL PUMP. - [SDR 2016FA0000228](https://openairdocs.org/sdr/2016FA0000228.md): Valve · stuck · May 11, 2016 · N914TD · Cirrus SR20 · Reciprocating Engine Cylinder Section > STUCK EXHAUST VALVE IN THE OPEN POSITION HAS CAUSED THE NR 5 CYLINDER PISTON TO PUSH IT CLOSED AND BENDING THE PUSHROD IN THE PROCESS. CYL ASSY'S NR 3, 5 & 6 DID THE SAME SHORTLY AFTER. CMI WAS CONTACTED & PARTS WERE COVEREND UNDER WARRANTY. REASON THIS WAS F - [SDR 2016FA0000168](https://openairdocs.org/sdr/2016FA0000168.md): Rotor Shaft · worn · Apr 6, 2016 · N581PU · Cirrus SR20 · DC Generator-Alternator > DURING A PHASE NR 2 INSPECTION TECH NOTED BROWN DUST COMING OUT OF NR 2 ALTERNATOR FAN AREA. WHEN ALTERNATOR WAS DISASSEMBLED FOR INSPECTION, DISCOVERED WEAR ON ROTOR SHAFT WHERE IT RIDES ON DRIVE END BEARING. BEARING WAS FREE TO ROTATE AND NO EXCESSIVE DRAG - [SDR 2016FA0000164](https://openairdocs.org/sdr/2016FA0000164.md): Bolt · broken · Apr 5, 2016 · N591PU · Cirrus SR20 · DC Generator-Alternator > ALTERNATOR NR 1 FAILED DURING A TRAINING FLIGHT. MAINTENANCE TECH NOTED A BROKEN ALTERNATOR CASE BOLT. THE CASE HALVES LOOSENED WHICH THEN CAUSED MORE DAMAGE WHEN THE ROTOR RUBBED THE STATOR, ALTERNATOR ES-4024LP. - [SDR CG9S2016FA0000121](https://openairdocs.org/sdr/CG9S2016FA0000121.md): Rotor Shaft · cracked · Mar 9, 2016 · N590PU · Cirrus SR20 · Magneto/Distributor > DURING MAGNETO 500 HOUR INSPECTION, DISCOVERED ROTOR SHAFT CRACKED AT KEYWAY FOR INTERNAL GEAR. THE KEY WAY AREA WAS ALSO CHIPPED FROM UNKNOWN REASONS. MAGNETO WAS 442 HOURS SINCE REBUILD. - [SDR 2016FA0000119](https://openairdocs.org/sdr/2016FA0000119.md): Bolt · broken · Mar 4, 2016 · N589PU · Cirrus SR20 · DC Generator-Alternator > DURING A PHASE 2 INSPECTION, TECH NOTED A BROKEN ALTERNATOR CASE BOLT. THE CASE HALVES HAD NOT LOOSENED UP AND NO FURTHER DAMAGE TO ALTERNATOR WAS NOTED. ALL THE CASE BOLTS WERE REPLACED WITH NEW. ALTERNATOR ES-4024LP. - [SDR 2016FA0000120](https://openairdocs.org/sdr/2016FA0000120.md): Bolt · broken · Mar 4, 2016 · N589PU · Cirrus SR20 · DC Generator-Alternator > DURING A PHASE 2 INSPECTION, THE TECH NOTED A BROKEN ALTERNATOR CASE BOLT. THE CASE HALVES HAD NOT LOOSENED UP AND NO FURTHER DAMAGE TO ALTERNATOR WAS NOTED. ALL THE CASE BOLTS WERE REPLACED WITH NEW. ALTERNATOR ES-4024LP. - [SDR CG9S2016022400096](https://openairdocs.org/sdr/CG9S2016022400096.md): Alternator · damaged · Feb 24, 2016 · N586PU · Cirrus SR20 · DC Generator-Alternator > DURING A TRAINING FLIGHT, IT WAS NOTED THE NR 2 ALTERNATOR WAS NOT FUNCTIONING. TROUBLESHOOTING BY MAINTENANCE DISCOVERED THE NUT FOR THE STATOR TERMINAL WAS MISSING AND THIS ALLOWED THE BOLT TO MIGRATE INTO THE CORE OF ALTERNATOR WHERE IT WAS CHEWED UP BY TH - [SDR CG9S2016022600097](https://openairdocs.org/sdr/CG9S2016022600097.md): Alternator · inoperative · Feb 22, 2016 · N595PU · Cirrus SR20 · DC Generator-Alternator > DURING A TRAINING FLIGHT, IT WAS NOTED THE NR 2 ALTERNATOR WAS NOT FUNCTIONING. INVESTIGATION BY MAINTENANCE DISCOVERED THE FIELD WAS OPEN ON ALTERNATOR. DURING REPLACEMENT IT WAS NOTED THE COOLING FAN AREA WAS COVERED WITH A DUSTING OF BRASS, COPPER COLORED - [SDR 2016FA0000088](https://openairdocs.org/sdr/2016FA0000088.md): Impulse Coupling · misinstalled · Feb 15, 2016 · N592PU · Cirrus SR20 · Magneto/Distributor > DURING 500 HOUR MAGNETO INSPECTION IT WAS NOTED THE IMPULSE COUPLING ON MAGNETO WAS NOT FUNCTIONING PROPERLY. UPON REMOVAL OF IMPULSE COUPLING IT WAS NOTED THAT THE DRIVE KEY WAS NOT INSTALLED IN DRIVE SHAFT PROPERLY AND WAS PROTRUDING AND JAMMING THE PROPER - [SDR 2015FA0000638](https://openairdocs.org/sdr/2015FA0000638.md): Pump · malfunctioned · Dec 9, 2015 · N594PU · Cirrus SR20 · Engine Fuel Pump > DURING A CIRRUS PROGRESSIVE INSPECTION PROGRAM PHASE 2 INSPECTION DISCOVERED ENGINE FUEL FLOW TO BE 15.7 GALLONS PER HOUR. THE PUMP WAS REPLACED. - [SDR 2015FA0000629](https://openairdocs.org/sdr/2015FA0000629.md): Keyway · worn · Dec 2, 2015 · N591PU · Cirrus SR20 · AC Generator-Alternator > DURING A PROGRESSIVE INSPECTION PROGRAM, 50 HOUR INSPECTION DISCOVERED ALTERNATOR NR 2 COOLING FAN LOOSE ON ALTERNATOR SHAFT. FAN PN: ES4137 IS PART OF ALTERNATOR, P/N: 653344. THE KEY WAY OF THE FAN HUB WEARS PREMATURELY ALLOWING ROTATIONAL MOVEMENT OF THE - [SDR CG9S2015112500618](https://openairdocs.org/sdr/CG9S2015112500618.md): Cam · cracked · Nov 25, 2015 · N594PU · Cirrus SR20 · Magneto/Distributor > DURING A MAGNETO 500 HR INSPECTION, DISCOVERED MAGNETO IMPULSE COUPLING CAM ASSY CRACKED AT KEYWAY. THIS MAGNETO WAS 442 HOURS SINCE ENGINE REMANUFACTURE. - [SDR 2015FA0000614](https://openairdocs.org/sdr/2015FA0000614.md): Alternator · inoperative · Nov 20, 2015 · N582PU · Cirrus SR20 · AC Generation System > PILOTS REPORTED ALTERNATOR NR 2 INOPERATIVE WITH ASSOCIATED CAS WARNING MESSAGE. TROUBLESHOOTING BY MAINTENANCE REVEALED HIGH RESISTANCE OF THE FIELD CIRCUIT OF THE ALTERNATOR WHEN ROTATED, SEEMED ACCEPTABLE WHEN STATIC. PERFORMED FULL FIELD CHECK OF ALTERNATO - [SDR 2015FA0000615](https://openairdocs.org/sdr/2015FA0000615.md): Cooling Fan · loose · Nov 18, 2015 · N584PU · Cirrus SR20 · AC Generator-Alternator > DURING A PROGRESSIVE INSPECTION PROGRAM, PHASE 2 INSPECTION DISCOVERED ALTERNATOR NR 2 COOLING FAN LOOSE ON ALTERNATOR SHAFT. FAN, PN: ES4137 IS PART OF ALTERNATOR, PN: 653344 MFG. THE KEY WAY OF THE FAN HUB WEARS PREMATURELY ALLOWING ROTATIONAL MOVEMENT OF - [SDR 2015FA0000589](https://openairdocs.org/sdr/2015FA0000589.md): Spring · broken · Nov 15, 2015 · N592PU · Cirrus SR20 · Engine Starter > PILOT REPORTED DURING ATTEMPTED ENGINE START, A GRINDING NOISE WAS HEARD AND PROPELLER DIDN'T TURN. DISCOVERED CLUTCH SPRING IN STARTER ADAPTER HAD BROKEN. - [SDR 2015FA0000594](https://openairdocs.org/sdr/2015FA0000594.md): Cooling Fan · loose · Nov 12, 2015 · N590PU · Cirrus SR20 · AC Generator-Alternator > DURING A CIRRUS PROGRESSIVE INSPECTION PROGRAM PHASE 2 INSPECTION DISCOVERED ALTERNATOR NR 2 COOLING FAN LOOSE ON ALTERNATOR SHAFT. FAN, PN: ES4137 IS PART OF ALTERNATOR, PN: 653344. THE KEY WAY OF THE FAN HUB WEARS PREMATURELY ALLOWING ROTATIONAL MOVEMENT O - [SDR 2015FA0000561](https://openairdocs.org/sdr/2015FA0000561.md): Cylinder Head · separated · Nov 11, 2015 · N487DA · Cirrus SR20 · Reciprocating Engine Cylinder Section > ACFT EXPERIENCED ENGINE OIL LOSS DURING CLIMB OUT, ACFT ALSO EXPERIENCED LOSS OF ENGINE OIL PRESSURE. ACFT LANDED SAFELY. UPON INSPECTION BY MAINTENANCE THE NR 5 CYLINDER HEAD WAS FOUND TO BE SEPARATED FROM THE CYLINDER BASE. - [SDR 2015FA0000590](https://openairdocs.org/sdr/2015FA0000590.md): Cooling Fan · loose · Nov 11, 2015 · N592PU · Cirrus SR20 · AC Generator-Alternator > DURING A PROGRESSIVE INSPECTION PROGRAM, PHASE 2 INSPECTION DISCOVERED ALTERNATOR NR 2 COOLING FAN LOOSE ON ALTERNATOR SHAFT. FAN PN: ES4137 IS PART OF ALTERNATOR PN: 653344. THE KEY WAY OF THE FAN HUB WEARS PREMATURELY ALLOWING ROTATIONAL MOVEMENT OF THE FAN - [SDR 2015FA0000592](https://openairdocs.org/sdr/2015FA0000592.md): Shaft · cracked · Nov 11, 2015 · N582PU · Cirrus SR20 · Magneto/Distributor > DURING MAGNETO 500 HOUR INSPECTION, DISCOVERED ROTOR SHAFT CRACKED NEAR DRIVE GEAR AT WOODRUFF KEY WAY. THIS MAGNETO WAS REMANUFACTURED WITH ONLY 442 HOURS SINCE REMAN. - [SDR 2015FA0000559](https://openairdocs.org/sdr/2015FA0000559.md): Keyway · worn · Nov 10, 2015 · N587PU · Cirrus SR20 · AC Generator-Alternator > DURING AN ACFT PROGRESSIVE 50 HOUR INSPECTION, DISCOVERED ALTERNATOR NR 2 COOLING FAN LOOSE ON ALTERNATOR SHAFT. THE FAN IS PART OF ALTERNATOR. THE KEY WAY OF THE FAN HUB WEARS PREMATURELY ALLOWING ROTATIONAL MOVEMENT OF THE FAN ON THE SHAFT. WE HAVE SEEN TH - [SDR CG9S2015FA0000550](https://openairdocs.org/sdr/CG9S2015FA0000550.md): Pump · malfunctioned · Nov 6, 2015 · N585PU · Cirrus SR20 · Engine Fuel Pump > DURING A CIRRUS PROGRESSIVE INSPECTION PROGRAM, PHASE 2 INSPECTION DISCOVERED ENGINE FUEL FLOW TO BE 13.8 GALLONS PER HOUR. THIS ACFT HAD BEEN FLOWN AN UNDERMINED NUMBER OF FLIGHTS WITH THE FUEL FLOW LOW. THIS RESULTED IN STUCK EXHAUST VALVES IN CYLINDERS NR - [SDR 2015FA0000546](https://openairdocs.org/sdr/2015FA0000546.md): Pump · low pressure · Nov 4, 2015 · N580PU · Cirrus SR20 · Engine Fuel Pump > PILOT REPORTED LOW FUEL FLOW ON CLIMB OUT IN THE RANGE OF 13.4 TO 13.6 GALLON 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. WHEN THE ALTITUDE - [SDR 2015FA0000557](https://openairdocs.org/sdr/2015FA0000557.md): Adapter · making metal · Nov 2, 2015 · N592PU · Cirrus SR20 · Engine Starter > DISCOVERED FERROUS METAL FLAKES IN OIL FILTER. DURING INVESTIGATION DETERMINED SOURCE WAS THE DRIVE SHAFT WITHIN THE STARTER ADAPTER. APPEARS THE DRIVE CLUTCH SPRING WAS DRAGGING ON THE DRUM AREA OF THE SHAFT REMOVING METAL FLAKES. - [SDR 2015FA0000547](https://openairdocs.org/sdr/2015FA0000547.md): Pump · low pressure · Nov 1, 2015 · N586PU · Cirrus SR20 · Engine Fuel Pump > PILOTS REPORTED LOW FUEL FLOW ON CLIMBOUT IN THE RANGE OF 14 GALLONS IAW HOUR. ESTABLISHED AN OPERATIONAL MINIMUM FUEL FLOW OF 16.0 GALLONS PER HOUR DUE TO OUR EXPERIENCE WITH THESE ENGINE DRIVEN FUEL PUMP ANEROID FAILURES. WHEN THE ALTITUDE COMPENSATING ANE - [SDR 2015FA0000593](https://openairdocs.org/sdr/2015FA0000593.md): Mount Bracket · cracked · Oct 13, 2015 · N581PU · Cirrus SR20 · AC Generator-Alternator > DURING A MFG PROGRESSIVE INSPECTION PROGRAM 50 HOUR INSPECTION, DISCOVERED THE NR 1 ALTERNATOR MOUNTING BRACKET CRACKED IN THE FORWARD ALTERNATOR MOUNTING HOLE. WE HAVE SEEN MANY OF THESE CRACK IN THIS SAME LOCATION. - [SDR 2015FA0000549](https://openairdocs.org/sdr/2015FA0000549.md): Pump · malfunctioned · Sep 21, 2015 · N584PU · Cirrus SR20 · Engine Fuel Pump > DURING A MFG PROGRESSIVE INSPECTION PROGRAM 50 HOUR INSPECTION, DISCOVERED ENGINE FUEL FLOW TO BE 13.9 GALLONS PER HOUR. IN THIS CASE WE WERE NOT ABLE TO ADJUST THE FUEL FLOW TO WITHIN LIMITS IAW CMI SID97-3F. PUMP WAS REPLACED. WE HAVE ESTABLISHED AN OPERATI - [SDR 2015FA0000548](https://openairdocs.org/sdr/2015FA0000548.md): Pump · malfunctioned · Sep 16, 2015 · N583PU · Cirrus SR20 · Engine Fuel Pump > DURING A PROGRESSIVE INSPECTION PROGRAM, 50 HOUR INSPECTION, DISCOVERED ENGINE FUEL FLOW TO BE 14.4 GALLONS IAW 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 ANEROI - [SDR 2015FA0000562](https://openairdocs.org/sdr/2015FA0000562.md): Pump · low pressure · Sep 3, 2015 · N588PU · Cirrus SR20 · Engine Fuel Pump > PILOTS REPORTED LOW FUEL FLOW ON CLIMBOUT AT 13 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 AN - [SDR 2015FA0000563](https://openairdocs.org/sdr/2015FA0000563.md): Pump · low pressure · Sep 2, 2015 · N582PU · Cirrus SR20 · Engine Fuel Pump > PILOTS REPORTED HIGHER THAN NORMAL CHT ON CYLINDERS NR 1 AND NR 3 ALONG WITH LOW FUEL FLOW ON CLIMB, IN THE RANGE OF 12 TO 14 GALLONS PER HOUR. WE HAVE ESTABLISHED AN OPERATIONAL MINIMUM FUEL FLOW OF 16.0 GALLONS IAW HOUR DUE TO OUR EXPERIENCE WITH THESE ENGI - [SDR 2015FA0000412](https://openairdocs.org/sdr/2015FA0000412.md): Rod · failed · Aug 26, 2015 · N24XT · Cirrus SR20 · Reciprocating Engine Power Section > ENGINE FAILURE IN FLIGHT. ROD WAS FOUND TO HAVE EXITED CRANK CASE. - [SDR 2015FA0000441](https://openairdocs.org/sdr/2015FA0000441.md): Pump · leaking · Aug 25, 2015 · Cirrus SR20 · Fuel Boost Pump > (B9582) LEAKING SEAL IN THE ELECTRIC FUEL PUMP. - [SDR 2015FA0000297](https://openairdocs.org/sdr/2015FA0000297.md): Engine · flamed out · Jun 28, 2015 · Cirrus SR20 · Engine (Turbine/Turboprop) > (B9739) ENGINE FLAMEOUT WHILE IDLE. - [SDR 2015FA0000296](https://openairdocs.org/sdr/2015FA0000296.md): Warning Light · illuminated · Jun 15, 2015 · Cirrus SR20 · Engine Fuel Distribution > (B9570) LOW FUEL FLOW WAS INDICATED. - [SDR 2015FA0000295](https://openairdocs.org/sdr/2015FA0000295.md): Warning Message · illuminated · Jun 14, 2015 · Cirrus SR20 · Engine Fuel Distribution > (B9581) LOW FUEL FLOW WAS INDICATED DURING TAKEOFF. - [SDR 2015FA0000302](https://openairdocs.org/sdr/2015FA0000302.md): Warning Message · illuminated · Jun 14, 2015 · Cirrus SR20 · Engine Fuel Distribution > (B9575) LOW FUEL FLOW AT IDLE ON THE GROUND. - [SDR 2015FA0000321](https://openairdocs.org/sdr/2015FA0000321.md): Distributor Blk · loose · Jun 8, 2015 · N8420F · Cirrus SR20 · Magneto/Distributor > COMPLAINT OF AN INTERMITTENT ENGINE VIBRATION. SUSPECTED AN IGNITION SYSTEM PROBLEM. FOUND 1 MAGNETO HAD JUMPED INTERNAL TIMING DUE TO DISTRIBUTOR BLOCK BEARING COMING LOOSE FROM THE BLOCK. OPENED THE SECOND MAGNETO, FOUND VIRTUALLY IDENTICAL DEFECT BUT IT - [SDR 2015FA0000301](https://openairdocs.org/sdr/2015FA0000301.md): Pump · low pressure · May 24, 2015 · Cirrus SR20 · Engine Fuel Pump > THE ENGINE DRIVEN PUMP PRODUCED LOW FUEL FLOW DURING TAKING OFF. - [SDR 2015FA0000289](https://openairdocs.org/sdr/2015FA0000289.md): Pump · leaking · May 22, 2015 · Cirrus SR20 · Engine Fuel Pump > FUEL PUMP FAILED AND THE ENGINE STOPPED DURING TAXI. - [SDR 2015FA0000300](https://openairdocs.org/sdr/2015FA0000300.md): Pump · low pressure · May 21, 2015 · Cirrus SR20 · Engine Fuel Pump > THE ENGINE DRIVEN FUEL PUMP PRODUCED LOW FUEL FLOW DURING TAKING OFF. Next page: https://openairdocs.org/engine/continental-io-360-es/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/engine/continental-io-360-es/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.