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 aircraft_model_key = 'T210N' 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 aircraft_model_key = 'T210N' 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 2024FA0000620Alternator · looseWE RECENTLY REPLACED AN ALTERNATOR DUE TO THE CHARGING SYSTEM DROPPING OUT IN FLIGHT, AND UPON EXAMINATION OF THE REMOVED ONE, IT WAS FOUND THAT TWO OF THE FOUR CASE SCREWS ARE LOOSE, BUT SAFETY WIRES ARE STILL IN PLACE. PLANE POWER MODEL ASG1200-1-PMA 24V , SDR 2017F00155Fuel Nozzle · cloggedPOWER LOSS AFTER TAKEOFF RESULTING IN RETURN TO AIRPORT. FUEL FLOW WAS REPORTED HIGH AND MANIFOLD PRESSURE NORMAL. SUSPECTED PARTIALLY PLUGGED FUEL INJECTOR NOZZLE.SDR 2015FA0000496Hub · crackedDURING ROUTINE INSPECTION, CRACKS WERE DISCOVERED IN THE HUB AT AFT EDGE, MATING SURFACE TO ENGINE CRANK FLANGE. THE MOST PROMINENT CRACK IS ABOUT .5" LONG. THERE IS NO DAMAGE HISTORY FOR THIS PROP. THE PROP IS INSTALLED UNDER STC SA3104SO TO AN ENGINE INSTASDR 2015FA0000493Coil · failedMAGNETO, SN 14020225 FAILED IN FLIGHT IN JULY 2014. PART TT APPROXIMATELY 16 HOURS. FOUND BAD CONDENSOR ON WARRANTY REPLACEMENT MAGNETO, SN 14020227, PART TT 184. FAILURES AT 16 AND 184 HOURS ARE UNUSUAL. BECAUSE MAGNETOS ARE OFTEN SOLD IN PAIRS IT IS POSSDR 2015FA0000492Condenser · failedFOUND BAD CONDENSOR ON MAGNETO, SN 14020225 IN JULY 2014. PART TT APPROXIMATELY 16 HOURS. ON OCTOBER 9, 2015 FOUND BAD CONDENSOR ON WARRANTY REPLACEMENT MAGNETO, SN 14020227, PART TT 184. FAILURES AT 16 AND 184 HOURS ARE UNUSUAL. BECAUSE MAGNETOS ARE OFTENSDR BGJA20150706001Circuit Breaker · failedTHE NAVIGATION LIGHTS CB FAILED. THE BREAKER FAILED IN SUCH A WAY THAT THE BREAKER REMAINED IN THE ON POSITION & COULD NOT BE TURNED OFF. THE CLIP INSIDE THE BREAKER HAD BROKEN FREE & THEN FALLEN DOWN INSIDE THE BREAKER WHERE IT HAD WEDGED ITSELF BETWEEN THESDR 2014FA0000558Fuel Line · leakingFUEL LINE HAS DARK STAIN HALF WAY BETWEEN ATTACHMENT AND FITTING. LINE PITTED UNDER PLASTIC ANTI-CHAFING MATERIAL, FUEL WEEP CAUSING STAIN. FOUND DURING ANNUAL.SDR BSYA2012063Indication Sys · malfunctionedON FINAL INTO ORL, PILOT WAS NOT GETTING GREEN DOWN & LOCK INDICATION AFTER GEAR WAS SELECTED DOWN. PILOT RECYCLED GEAR & HAND PUMPED, NO HELP. PILOT DID A FLY BY THE TOWER TO VERIFY GEAR WAS DOWN. PILOT PROCEEDED TO LAND AT ORL, GREEN DOWN & LOCK INDICATIOSDR 2013FA0000573Rudder Bar · brokenDURING TAXI PILOT WAS ATTEMPTING TO CENTER THE NOSE WHEEL FOR RUN-UP PRIOR TO TAKE-OFF. WHEN PILOT PUSHED LEFT RUDDER PEDAL A LOUD POP WAS HEARD FOLLOWED BY THE LEFT PEDAL GOING LIMP. CO-PILOT STILL HAD FULL CONTROL ON HIS SIDE. CO-PILOT THEN TAXIED BACK TO RASDR 2013FA0000320Alternator · inoperativeACFT LOST ALL ELECTICAL OPERATION IN FLIGHT. ACFT RETURNED TO DEPARTED AIRPORT AND MADE A MANUEL GEAR EXTENTION LANDING AND SAFE ROLL OUT TO THE PARKING RAMP. MX INSPECTED AND TROUBLESHOOT PROBLEM AND FOUND A DEFECTIVE ANTERNATOR. R & R ALTERNATOR WITH O/H SDR CKE2013F00000Bushing · looseFUEL INJECTOR BUSHINGS DID NOT STAY IN PLACE WHEN FUEL INJECTORS WERE REMOVED. INJECTORS WERE REMOVED FOR CLEANING. THIS ENGINE HAS 185 TSMOH AND 5 OUT OF THE 6 BUSHINGS LOOSENED WITH THE INJECTOR. PROBABLE CAUSE IS THAT THE LOCTITE 620 DOES NOT HOLD THE BUSDR 2013FA0000014Cylinder Head · crackedCOMPRESSION CHECK AT ANNUAL REVEALED CRACKED HEAD-AD 2004-08-10 NA DUE TO SN AND "A" STAMP. THIS CYLINDER SEEMS TO HAVE SAME PROBLEM AS AD BUT WAS INT INCLUDED. NOTIFIED MFG. AD MAY NEED TO BE EXPANDED. FURTHER TESTING WITH SCRAP AND WATER. REVEALED 4 MORSDR 2013FA0000013Cylinder Head · crackedCOMPRESSION CHECK AT ANNUAL REVEALED CRACKED HEAD-AD 2004-08-10 NA DUE TO SN AND "A" STAMP. THIS CYLINDER SEEMS TO HAVE SAME PROBLEM AS AD BUT WAS INT INCLUDED. NOTIFIED MFG. AD MAY NEED TO BE EXPANDED. FURTHER TESTING WITH SCRAP AND WATER. REVEALED 4 MORSDR 2013FA0000012Cylinder Head · crackedCOMPRESSION CHECK AT ANNUAL REVEALED CRACKED HEAD-AD 2004-08-10 NA DUE TO SN AND "A" STAMP. THIS CYLINDER SEEMS TO HAVE SAME PROBLEM AS AD BUT WAS NOT INCLUDED. NOTIFIED MFG. AD MAY NEED TO BE EXPANDED. FURTHER TESTING WITH SCRAP AND WATER. REVEALED 4 MORSDR 2013FA0000011Cylinder Head · crackedCOMPRESSION CHECK AT ANNUAL REVEALED CRACKED HEAD-AD 2004-08-10 NA DUE TO SN AND "A" STAMP. THIS CYLINDER SEEMS TO HAVE SAME PROBLEM AS AD BUT WAS INT INCLUDED. NOTIFIED MFG. AD MAY NEED TO BE EXPANDED. FURTHER TESTING WITH SCRAP AND WATER. REVEALED 4 MORSDR 2013FA0000010Cylinder Head · crackedCOMPRESSION CHECK AT ANNUAL REVEALED CRACKED HEAD-AD 2004-08-10 NA DUE TO SN AND "A" STAMP. THIS CYLINDER SEEMS TO HAVE SAME PROBLEM AS AD BUT WAS INT INCLUDED. NOTIFIED MFG. AD MAY NEED TO BE EXPANDED. FURTHER TESTING WITH SCRAP AND WATER. REVEALED 4 MORSDR 2013FA0000009Cylinder Head · crackedCOMPRESSION CHECK AT ANNUAL REVEALED CRACKED HEAD-AD 2004-08-10 NA DUE TO SN AND "A" STAMP. THIS CYLINDER SEEMS TO HAVE SAME PROBLEM AS AD BUT WAS INT INCLUDED. NOTIFIED MFG. AD MAY NEED TO BE EXPANDED. FURTHER TESTING WITH SCRAP AND WATER. REVEALED 4 MORSDR 2012FA0000222Contactor · shortedPILOT REPORTED THAT ON LANDING, ACFT LOST ALL ELECTRICAL POWER. PERFORMED INSP AND TROUBLESHOOTING. FOUND BATTERY, STARTER AND STARTER RELAY AT FAULT. ACFT HAD A BURNED WIRE, ELECTRICAL ODOR. FOUND THAT THE STARTER STAYED ENGAGED AND IT ACTED LIKE AN ELECTSDR 2012FA0000221Battery · damagedPILOT REPORTED THAT ON LANDING, ACFT LOST ALL ELECTRICAL POWER. PERFORMED INSP AND TROUBLESHOOTING. FOUND BATTERY, STARTER AND STARTER RELAY AT FAULT. ACFT HAD A BURNED WIRE, ELECTRICAL ODOR. FOUND THAT THE STARTER STAYED ENGAGED AND IT ACTED LIKE AN ELECTSDR 2012FA0000220Starter · burnedPILOT REPORTED THAT ON LANDING, ACFT LOST ALL ELECTRICAL POWER. PERFORMED INSPECTION AND TROUBLESHOOTING. FOUND BATTERY, STARTER AND STARTER RELAY AT FAULT. ACFT HAD A BURNED WIRE, ELECTRICAL ODOR. FOUND THAT THE STARTER STAYED ENGAGED AND IT ACTED LIKE ANSDR SQP2011F00000Cylinder Head · separatedPILOT REPORTED LOUD BANG ON CLIMBOUT. RETURNED WITHOUT INCIDENT TO FIELD. UPON EXAMINATION FOUND NR 4 CYLINDER HEAD SEPARATED FROM CYLINDER AT 5TH COOLING FIN ON HEAD. ENGINE TSO AND CYLINDER TSN 817.6 HRS. LAST COMPRESSION CHECK WAS AT 100 HR INSPECTION 1SDR 2010FA0001213Rod Bolt · loosePILOT EXPERIENCED ENGINE SUDDEN STOPPAGE IN FLIGHT AND MADE UNSCHEDULED LANDING. ANALYSIS OF THE CATASTROPHIC ENGINE FAILURE INDICATED FAILURE OCCURED WHEN THE NR5 CONNECTING ROD SEPARATED. THE CAUSE OF FAILURE OF THE CONNECTING ROD WAS A LOOSE ROD BOLT IN THESDR 2010FA0001177Case · puncturedPILOT REPORTED LOSSING OIL PRESSURE FOLLOWED BY LOSS OF POWER. AFTER FORCED LANDING ON DIRT ROAD, INSP SHOWED CONNECTING ROD HAD PENETRATED UPPER LT SIDE OF MAIN CASE.SDR 2010FA0000937Stop Pin · missingPILOT REPORTED ENGINE WOULD NOT SHUTDOWN WITH MIXTURE LEAN, UPON INSP OF CAUSE, FOUND MIXTURE STOP PIN MISSING AND HAD FALLEN OUT DURING OPERATION.SDR 2010FA0000719Stator · failedSTATOR POST ON ALTERNATOR FELL OUT IN FLIGHT, ALTERNATOR FAILED AFTER 44 HOURS SINCE O/H.SDR 2010FA0000030Adapter · brokenDURING 100HR INSP FOUND GEAR TOOTH IN OIL SUMP DRAIN PLUG. INVESTIGATED, FOUND STARTER DRIVE TOOTH BROKEN AND MATCHED TOOTH TO GEAR. NO FURTHER DAMAGE NOTED.SDR FPI2009F00000Attach Bracket · crackedCRACK FOUND IN LT HORIZONTAL STAB BRACE. FOUND DURING 100 HR PHASE INSP.SDR 2008FA0000894Pump · shearedON SECOND TEST FLIGHT AFTER FACTORY REBUILT ENG INSTALLATION, ENG QUIT DURING TAKEOFF, JUST AFTER LIFTOFF, ALTITUDE LESS THAN 5 FT AGL. PILOT LANDED ACFT AND ROLLED OUT WITHOUT FURTHER INCIDENT. DURING THIS EVENT, PILOT REPORTED THAT AT TAKEOFF INITIATION, POWSDR 2008FA0000443Guide · out of toleranceAFTER NUMEROUS ATTEMPTS TO TROUBLESHOOT FREQUENT ENGINE MISFIRES OCCURRING PRIMARILY IN THE INITIAL CLIMB STAGES OF FLIGHT, THE ENGINE VALVE TRAIN WAS INSPECTED FOR STICKING VALVES. DIMENSIONAL INSPECTIONS OF THE EXHAUST VALVE GUIDES IN ALL 6 CYLINDERS REVEALSDR 2008FA0000107Powerpack · wornSMOKE IN COCKPIT, GEAR NOT FULLY RETRACTED, EXTENDED OK. FOUND HYDRAULIC POWERPACK MOTOR (ORIGINAL) WORNOUT. REMOVED AND REPLACED WITH O/H UNIT. OPS, OK.SDR 2007FA0000641Line · mismanufacturedNEW FUEL INJECTOR LINE NR 5 CYL RAM PMA REPLACEMENT. INSTALLED ON ENGINES, WELD DEFECT ALLOWED DEVIPER END BAIL TO COME LOOSE FROM LINE. NOTED FUEL LEAN ON TOP OF ENGINE AT ANNUAL 100 HR INSP. (K)SDR 2007FA0000399Magneto · corrodedEMERGENCY RETURN TO FIELD: INSPECTION REQUIREMENTS FOR MAGNETO (PN 6320) ARC NOT ADEQUATE TO INSURE PROPER VENTING (PRESSURIZED MAG). SB2-80C SPECIFIES ONLY EXTERNAL INSPECTION IS REQUIRED EVERY 100 HOURS AND AN INTERNAL INSPECTION AFTER 500 HOURS. THE SUBESDR 2007FA0000398Magneto · corrodedEMERGENCY RETURN TO FIELD: INSPECTION REQUIREMENTS FOR MAGNETO (PN 6320) ARC NOT ADEQUATE TO INSURE PROPER VENTING (PRESSURIZED MAG). SB 2-80C SPECIFIES ONLY EXTERNAL INSPECTION IS REQUIRED EVERY 100 HOURS AND AN INTERNAL INSPECTION AFTER 500 HOURS. THE SUBSDR 2006FA0001202Turbocharger · failedNEW TURBO ASSY WAS INSTALLED 6/30/06. FOUR MONTHS LATER ON 10/6/06 (41 HOURS TT) THE TURBO SHAFT TIGHTENED UP ENOUGH TO NOT PRODUCE TAKEOFF POWER ON NEXT FLIGHT. OIL PRESSURE AND OIL VOLUME DELIVERED TO TURBO BEARINGS WAS VERIFIED TO BE ADEQUATE. CUSTOMER PSDR 2006FA0000718Elt · inoperativeFOUND ELT TOTALLY INOPERATIVE DURING ANNUAL INSPECTION, BATTERY VOLTAGE OK. UNABLE TO DETERMINE IF IMPACT SWITCH WAS ALSO INOPERATIVE. (K)SDR 2006FA0001201Turbocharger · failedNEW TURBO ASSY WAS INSTALLED 3/27/2006. (3) MONTHS LATER ON 6/30/06 (32 HOURS TT) THE TURBO SHAFT TIGHTENED UP ENOUGH TO NOT PRODUCE TAKEOFF POWER ON NEXT FLIGHT. OIL PRESSURE AND OIL VOLUME DELIVERED TO TURBO BEARINGS WAS VERIFIED TO BE ADEQUATE. CUSTOMER SDR 2006FA0000514Cylinder · erodedFOUND NR 6 PISTON ERODED FROM POSSIBLE DETONATION BY UNKNOWN CAUSES. FOUND NR5 CYLINDER CONNECTING ROD CAP MISSING AND INTERNAL DAMAGE TO THE CRANKCASE. NO OIL WAS NOTED ON THE DIPSTICK PRESUMED TO BE FORCED OUT OF THE ENGINE DUE TO EXCESSIVE BLOW BY FROM THSDR 2006FA0001070Bearing · seizedOVERHAULER W/O NR 84062, O/H DATE 10/06/2006. STARTER BEARING SEIZED AFTER INSTALLATION STARTER MOTOR FAILED. (K)SDR CA060201001Spar · crackedA 100 HR INSPECTION WAS STARTED A CRACK WAS DISCOVERED AT THE RIGHT FRONT SPAROUT BOARD END WHERE IT ATTACHES TO THE SUB SPAR. THE CRACK IS VERTICAL RUNNING APPROXIMATELY 1 1/2 TO TWO INCHES IN LENGTH. THE CRACK STARTS AT THE TOP AND RUNS DOWN THROUGH A RIVESDR 2005FA0001242Pin · backed outTHE PIN THAT HOLDS THE DRIVE GEAR ONTO THE ACTUATOR DRUM HAD FALLEN OUT WHEN THE AIRCRAFT WAS TRIMMED NOSE UP. THE PILOT HAD TO PUSH ON THE YOKE WITH GREAT FORCE TO PITCH THE AIRCRAFT DOWN. AFTER EXAMINING THE ACTUATOR I NOTICED THAT THE HOLE FOR THE PIN WAS ESDR 2005FA0001238Pin · backed outTHE PIN THAT HOLDS THE DRIVE GEAR ONTO THE ACTUATOR DRUM HAD FALLEN OUT WHEN THE AIRCRAFT WAS TRIMMED NOSE UP. THE PILOT HAD TO PUSH ON THE YOKE WITH GREAT FORCE TO PITCH THE AIRCRAFT DOWN. AFTER EXAMINING THE ACTUATOR, NOTICED THAT THE HOLE FOR THE PIN WAS ESDR 2005FA0001204Alternator · seizedAIRCRAFT WAS RUN UP PRIOR TO 50 HOUR INSPECTION AND NO DEFECTS WERE FOUND DURING RUN UP. AFTER INSPECTION, PERFORMED POST INSPECTION RUN AND NOTICED A LOUD SQUEALING NOISE AND SMOKE COMING FROM ENGINE COMPARTMENT. ENGINE WAS SHUTDOWN AND INSPECTION REVEALED THSDR 2005FA0001133Cylinder Head · damagedDURING CRUISE FLIGHT, A LOUD BANG FROM THE ENGINE COMPARTMENT WAS FOLLOWED BY LOSS OF POWER AND SIGNIFICANT ENGINE VIBRATION. THE PILOT MADE AN EMERGENCY LANDING ON A DIRT ROAD WITH NO DAMAGE TO THE AIRCRAFT. THE NR 1 CYLINDER HEAD HAD FRACTURED COMPLETELY TSDR 2005FA0000999Cylinder Head · separatedNR 2 CYLINDER HEAD SEPARATED FROM BARREL. OCURRENCE OCCURRED DURING DEPARTURE FROM AIRPORT, ENROUTE. PROBABLE CAUSE IS WORN CYLINDER OR POSSIBLE OVERBOOST. RECOMMEND WHEN PERFORMING COMPRESSION TEST THAT YOU PRESSURIZE AND SOAP CYLINDER AT BARREL AND HEAD ASDR 2005FA0000586Governor · pluggedDEPARTING SOFT FIELD POWER AND RPM FINE ON INITIAL ROLL. AFTER WHEELS BECAME LIGHT, POWER BLED OFF, YIELDING NO FURTHER ACCELERATION OR LIFT. ABORTED TAKE-OFF, NOSE WHEEL GOUGED INTO SOFT SAND, BREAKING NOSE FORK, PITCHING NOSE OF AIRCRAFT INTO DIRT. PROP BSDR 2005FA0000580Encoder · erraticALTITUDE OUTPUT BECAME ERRATIC, VARYING SEVERAL HUNDRED FT BOTH ABOVE AND BELOW THE ACTUAL ALTITUDE OVER A PERIOD OF 30 MINUTES. PROBABLY CAUSED BY INTERMITTENT HEATER THERMOSTAT.SDR 2005FA0000216Connecting Rod · failedNR 2 CONNECTING ROD FAILED BREAKING CRANKCASE, KNOCKING LT MAG FROM MOUNT. ROD SHOWED FRICTION WELDING TO CRANK PRIOR TO FAIURE. COUNTERWEIGHT DAMAGED BY IMPACT WITH ROD. APPEARS ENG CONTINUED TO OPERATE BRIEFLY FOLLOWING ROD SEIZURE. PILOT ACCOMPLISHED SUSDR B3OR20040719Hinge · looseANNUAL INSP, ALTERNATE AIR SOURCE DOOR WAS LOOSE. MECHANIC FOUND DOOR SPRING P/N 1250728-1, HINGE PIN P/N MS20253P2-364 IN INDUCTION AIR BOX DUCTING. PIN AND SPRING WERE RE-ASSEMBLED WITH DOOR. WHEN PARTS WERE RE-ASSEMBLED, BOTH UPPER AND LOWER ENDS OF HINGESDR CA050125015Piston · disintegrated(CAN) ENGINE HAD 450 HOURS SINCE TOTAL O/H, WAS PERFORMING NORMAL. CYL LEAK TEST WERE MIN. 60/80 AND OIL CONSUMPTION WAS 1 LT-13 HRS. AC WAS IN BASE LEG WITH POWER REDUCED GRADUALLY BACK TO 20 IN., PROP NEAR FINE, MIXTURE NEAR RICH. VIBRATION STARTED IN ENGSDR B3OR20040709Line · cutPILOTS ENTERED THE AC AND TAXIED DOWN THE TAXIWAY. AS BRAKES WERE BEING APPLIED, IT WAS NOTICED THAT RT BRAKE WAS NOT OPERATING. AC EXITED TAXI WAY AT A LOW SPEED CAME TO A STOP IN ABOUT FOUR INCHES OF MUD ALONGSIDE OF TAXIWAY. THERE WAS NO DAMAGE TO AC OR PRO
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