Continental IO-360-E
Service difficulty reports · 18
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 = 'IO360E' 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 = 'IO360E' 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 2021FA0000328Tachometer · frozenLEFT ENGINE TACHOMETER HOURS REPORTING FAILED / STOPPED REPORTING TACH HOURS.SDR CA071031005Tube · damaged(CAN) INTAKE PIPE ON NR 1 CYLINDER FLANGE DAMAGED. (TC NR 20071031005)SDR AU510001762Alternator · failed(AUS) ALTERNATOR FAILED. INVESTIGATION FOUND STATOR TO DIODE FEEDER WIRES CHAFING ON HOUSING AND SHORTED. BRUSH WIRE TAIL FOUND TO BE RUNNING ON STATOR BRUSH RING. (CASA NR 510001762)SDR AU510002057Magneto · failed(AUS) LT AND RT MAGNETOS PREMATURELY WORN. LT MAGNETO, HIGH VOLT CONTACT TERMINALS IN DIST BLOCK/CAP ARE ERODED/ARCED. HIGH VOLT DIST ARM TIP HAS ERODED CENTER WIPER ELECTRODE, ARCED END W/PITTING, MATERIAL BREAK DOWN. POINTS SHOW SIGNS OF PITTING WITHIN SESDR AU510002064Alternator · failed(AUS) ALTERNATOR FAILED. INVESTIGATION FOUND DEFECTIVE INSULATORS AND BATTERY POST TO ALTERNATOR BODY ARCING. (CASA NR 510002064)SDR AU510002149Piston · damagedNR 3 CYLINDER SEVERELY DAMAGED. INVESTIGATION CONTINUING.SDR AU510002183Line · damaged(AUS) FUEL PIPES PN 11443-005 AND PN 11444-005 CRACKED/DAMAGED ON FLARES AT THE (T) FITTING ENDS. SWARF WAS ALSO FOUND ON THE FLARES. (CASA NR 510002183)SDR AUS20040445Seat Belt · faulty(AUS) PILOTS SEAT BELT SHOULDER HARNESS DOES NOT FULLY RETRACT INTO INERTIA REEL. INVESTIGATION FOUND A STOP INSTALLED IN THE WEBBING IN AN AREA JUST BELOW JUNCTION.SDR AUS20030940Door Frame · cracked(AUS) LT ENTRY DOOR FRAME PN 12843003 AND RT ENTRY DOOR FRAME PN 12843004 CRACKED IN AREA ABOVE SIDE WINDOW. CRACK LENGTHS APPROXIMATELY 457.2MM (18IN).SDR CA030513001Bracket · cracked(CAN) FORWARD ALTERNATOR MOUNTING BRACKET CRACKED. THE CRACK IS LOCATED ON THE BOTTOM SIDE OF THE FORWARD ALTERNATOR MOUNTING HOLE.SDR 2003FA0000486Crankcase · crackedTWO ONE INCH CRACKS WERE FOUND ON THE FORWARD, RT SIDE OF THE ENGINE CRANKCASE. THE CRACKS ARE LOCATED AROUND THE FRONT ALTERNATOR MOUNTING BRACKET. TOP REAR CASE THROUGH BOLT. THIS IS THE THIRD AIRCRAFT WER ARE DOING AN ENGINE CHANGE ON WITH THIS DISCREPANSDR 2003FA0000461Engine · malfunctionedAIRCRAFT ENGINE DID NOT RESPOND TO FULL THROTTLE DURING ATTEMPTED REJECTED LANDING FOLLOWING ENCOUNTER WITH SEVERE LOW ALTITUDE TURBULENCE. SUBSEQUENT EXAMINATION OF ENGINE AND COMPONENTS REVEALED NO ABNORMALIES. RECOMMEND CAUTIONARY NOTE IN PILOT OPERATING SDR 2003FA0000201Crankcase · crackedON AIRCRAFT, BECAUSE OF A CRACK FOUND ON ANOTHER ENGINE, DECIDED TO INSPECT AND FOUND A CRACK ON THE RIGHT FRONT SIDE OF THE ENGINE CASE AT THE ALTERNATOR MOUNTING FLANGE AREA. THE CRACK STARTED ON THE ALTERNATOR REAR MOUNTING CASE THROUGH BOLT. THIS CRACK ISDR 2003FA0000202Crankcase · crackedA SLIGHT OIL LEAK COMING FROM THE FRONT RIGHT SECTION OF THE ENGINE WAS FOUND TO BE A CRACKED CASE. REMOVED NR 1 ALTERNATOR AND DYE CHECKED THE AREA. FOUND A 6 INCH CRACK ON THE ALTERNATOR MOUNTING FLANGE STARTING ON THE ALTERNATOR MOUNTING FLANGE THROUGH BOSDR 2001FA0000557Crankshaft · failedIN FLIGHT ENGINE FAILURE, CRANKSHAFT COUNTERWEIGHT AND DOUBLE ROD FAILURE, BLEW TWO ROD THROUGH CASE.(K)SDR 20010322CW012Cartridge · jammedON RUN UP & PREPARING FOR FLIGHT, ELEVATOR DOWN AUTHORITY COULD NOT BE ACHIEVED UNDER NORMAL CONTROL PRESSURE. PILOT RETURNED AND GROUNDED THE AIRCRAFT FOR MAINTENANCE. INVESTIGATION IDENTIFIED BINDING TO BE LOCATED WITHIN THE PITCH TRIM CARTRIDGE ASSEMBLY PSDR 95ZZZX5230Magneto · failedENGINE INTERMITTENTLY RUNNING ROUGH. MAGNETOS BOTH HAD 1,786 HOURS SINCE INSTALLATION. SABOTAGE PAINT APPLIED BY MANUFACTURER WAS NOT DISTURBED INDICATING NO 500-HOUR INSPECTIONS HAD BEEN PERFORMED. INSPECTION SHOWED TRACES OF 'CROSS-FIRING' IN DISTRIBUTOR SDR 95ZZZX5231Magneto · failedENGINE INTERMITTENTLY RUNNING ROUGH. MAGNETOS BOTH HAD 1,786 HOURS SINCE INSTALLATION. SABOTAGE PAINT APPLIED BY MANUFACTURER WAS NOT DISTURBED INDICATING NO 500-HOUR INSPECTIONS HAD BEEN PERFORMED. INSPECTION SHOWED TRACES OF 'CROSS-FIRING' IN DISTRIBUTOR
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