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 = '402C' 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 = '402C' 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 97ZZZX4143Gusset · crackedCRACKS FOUND IN PLT SEAT SUPPORT STRUCTURE BELOW FLOOR AT TOP SIDE OF GUSSETS. INBOARD AND OUTBOARD SUPPORT CRACKS WERE FOUND AT FLOOR LINE. SUBMITTER RECOMMENDS INSTALLING DOUBLERS INSIDE AT TOP AND AFT SIDES OF NEW GUSSETS OR MANUFACTURE GUSSETS OF HEAVIERSDR 97ZZZX4142Gusset · crackedCRACKS FOUND IN SEAT (PLT) SUPPORT STRUCTURE BELOW FLOOR AT TOP SIDE OF GUSSETS INBOARD AND OUTBOARD SUPPORT. CRACKS WERE FOUND AT FLOOR LINE. SUBMITTER RECOMMENDED INSTALLING DOUBLERS INSIDE AT TOP AND AFT SIDES OF NEW GUSSETS OR MANUFACTURE GUSSETS OF HEAVSDR 97ZZZX4141Gusset · crackedCRACKS FOUND IN SEAT (PLT) SUPPORT STRUCTURE BELOW FLOOR AT TOP SIDE OF GUSSETS INBOARD AND OUTBOARD SUPPORT. CRACKS WERE FOUND AT FLOOR LINE. SUBMITTER RECOMMENDED INSTALLING DOUBLERS INSIDE AT TOP AND AFT SIDES OF NEW GUSSETS OR MANUFACTURE GUSSETS OF HEAVSDR P77A9700183Elbow · no threadsPILOT REPORTED DURING FLIGHT, RT MAP STARTED DROPPING. PILOT GOT WORRIED, SHUT DOWN RT ENGINE AND FEATHERED PROPELLER. INVESTIGATION FOUND ELBOW ON INDUCTION TUBE FOR MAP GAUGE BLEW OUT. FIRST 5 THREADS OF ELBOW MISSING, REPLACED ELBOW. GROUND RUNS. ALL OSDR 97ZZZX3406Rod End · bearing failedNOSE GEAR COLLAPSED UPON LANDING. THE NOSE GEAR ROD END BEARING SEPARATED FROM HOUSING ALLOWING NOSE GEAR TO BECOME SEPARATED FROM NOSE GEAR ACTUATOR. THIS ALLOWED ACTUATOR TO FULLY EXTEND AND GIVE THE PILOT THE APPEARANCE OF 3 GREEN, DOWN, AND LOCKED, BUT, SDR AU970801Battery · cracked(AUS) ELT BATTERY PACK CRACKED AND LEAKING - ELT BATTERY MOUNTING TRAY AND STRUCTURE BENEATH ELT CONTAMINATEDSDR AU970815Wire · shorted(AUS) LANDING GEAR SELECTOR WIRE SHORT CIRCUITED IN AREA BEHIND INSTRUMENT PANELSDR CA970620007Relief Valve · misaligned(CAN) A NEWLY INSTALLED ENGINE HAD OIL PRESSURE PROBLEMS. THE LOW OIL PRESSURE AT IDLE WAS FOUND TO BE CAUSED BY THE OIL PRESSURE ADJUSTING SCREW BEING MISALIGNED WITH THE HOUSING CAUSING THE VALVE NOT TO SEAT SQUARELY. THE REPLACEMENT OF THE OIL PRESSURE RELISDR CA970527010Fork Tube · broken(CAN) AME NOTICED THE RIGHT HAND LOWER AXLE ATTACH POINT WAS BROKEN. DAMAGE APPEARS TO HAVE BEEN CAUSED BY A BEARING SEIZURE.SDR 97ZZZX2796Angle · failedDURING SCHEDULED INSPECTION OF NOSE WHEELWELL UPPER AREA, LEFT ANGLE WAS DISCOVERED BROKEN CAUSING DAMAGE TO ADJACENT PANELS AND STRUCTURE. IT APPEARED ANGLE HAD BEEN REPAIRED WITH A SPLICE. HOWEVER, SPLICED AREA FAILED. ANGLE WAS REPLACED AND STRUCTURE REPSDR AU970886Valve · failed(AUS) LANDING GEAR BLOWDOWN BOTTLE OUTLET VALVE FAULTY - INVESTIGATION FOUND THAT THE `O' RING ON THE VALVE POPPET ASSEMBLY WAS MISSING- REMAINS OF THE `O' RING WERE FOUND DOWNSTREAM IN THE EMERGENCY GEAR BLOWDOWN SYSTEMSDR AU970887Valve · faulty(AUS) HYDRAULIC MANIFOLD VALVE FAULTY - DURING STRIPDOWN OF THE VALVE PIECES OF `O' RING WERE FOUND - SUSPECT `O' RING CAME FROM THE EMERGENCY GEAR DOWN BOTTLE PNO 9910154-3 (MDR 97/0886)SDR 97ZZZX1839Line · crackedFOUND PRESSURE LINE 5100111-71 CRACKED IN A BEND. CRACK ALLOWED ALL HYDRAULIC FLUID TO PUMP OVERBOARD. THE FAILURE POINT OF THE LINE IS AFT OF THE ENGINE FIREWALL WITH NO DIRECT ACCESS FOR INSPECTION. THE FAULT WAS FOUND WHEN THE LINE WAS REMOVED FOR TROUBLSDR CA970407016Vacuum Pump · faulty(CAN) REPORT OF #2 ENGINE VACUUM PUMP INOPERATIVE. PUMP REMOVED AND COMPOSITE SHAFT/SPLINE FOUND SHEARED. OVERHAULED VACUUM PUMP INSTALLED.SDR CA970325002Cylinder Assy · cracked(CAN) DURING INSPECTION FUEL STAINS WERE FOUND ON ONE CYLINDER OF THE LH ENGINE AND ONE CYLINDER OF THE RH ENGINE IN THE AREA OF THE COOLING FINS. FURTHER INSPECTION FOUND THE CYLINDERS WERE CRACKED. MAINTENANCE HAVE CONCLUDED THE CYLINDERS ARE CRACKING AS A ASDR 97ZZZX1227Diode · burntPILOT REPORTED ARCING AND SMOKE FROM ELECTRIC HEATED WINDSHIELD. ELECTRICAL CONNECTION OR LEFT SIDE OF HEATED WINDSHIELD HAS DIODE THAT MELTED AND ARCED.SDR 97ZZZX1229Aileron · weight brokenAILERON HAS A 4 FOOT LEAD WEIGHT INSTALLED FOR BALANCING. LEAD WEIGHT HAD BROKEN AWAY FROM MOUNT AND WAS LOOSE IN LEADING EDGE OF AILERON. LEADING EDGE WAS REMOVED AND BALANCE WEIGHT WAS RE-ATTACHED TO AILERON. FLIGHT CONTROL WAS RE-BALANCED AND RETURNED TOSDR 97ZZZX1823Crankcase · crackedOIL LEAK. FOUND RIGHT CRANKCASE CRACKED IN THE MIDDLE OF THE REAR MOUNTING FLANGE OF THE ALTERNATOR. CRACK EXTENDED TOWARDS THE NR 4 MAIN BEARING 45MM (1.75 INCH). LOOKING FROM THE OUTSIDE, THE CRACK ALSO EXTENDS TOWARDS THE BACK 25MM (1 INCH) DIRECTLY UNDESDR AU970082Torque Link · stiff(AUS) NOSE LANDING GEAR TORQUE LINKS STIFF IN OPERATION DUE TO THE LOWER ATTACHMENT BOLT BEING OVERTORQUED - NOSE OLEO WOULD NOT FULLY EXTEND CAUSING NLG TO FOUL ON GEAR DOORS -PERSONNEL/MAINTENANCE ERRORSDR 97ZZZX754Pump · failedBOOST PUMP INOPERATIVE UPON TRYING TO PRIME ON INITIAL START OF THE DAY. INSTALLED OVERHAULED BOOST PUMP. OPS CHECKED OK.SDR 97ZZZX1824Tach Generator · ear brokenTACHOMETER GENERATOR AREA WAS OILY. TACHOMETER WAS REMOVED FOR INSPECTION. FOUND ONE OF THE EARS OF THE GENERATOR SHAFT FORK BROKEN OFF. NO OPINION AS TO CAUSE.SDR AU970105Selector Valve · faulty(AUS) LANDING GEAR SELECTOR VALVE FAULTY - REPAIRED ITEM HAD BEEN FITTED BEFORE THE PREVIOUS FLIGHT - THE VALVE WAS AGAIN RETURNEDTO THE OVERHAUL FACILITY - THE VALVE COULD NOT BE FAULTED INITIALLY BUT AFTER REPEATED TESTING THE VALVE FAILED - SUSPECT FAULTY SSDR 97ZZZX553Gusset · crackedINSP OF THE PILOT SEAT SUPPORT STRUCTURE FOUND P/N 5011011-7 GUSSETT, P/N 5015019-1, AND 5015019-3 CHANNELS HAD CRACKED AND FAILED. THERE IS NO ACCESS TO P/N 501101107 FOR INSPECTION AND IT IS BELIEVED THIS PART FAILED FIRST PUTTING HEAVY LOAD ON CHANNELS.SDR 97ZZZX552Channel · crackedINSP OF THE PILOT SEAT SUPPORT STRUCTURE FOUND P/N 5011011-7 GUSSETT, P/N 5015019-1, AND 5015019-3 CHANNELS HAD CRACKED AND FAILED. THERE IS NO ACCESS TO P/N 501101107 FOR INSPECTION AND IT IS BELIEVED THIS PART FAILED FIRST PUTTING HEAVY LOAD ON CHANNELS.SDR 97ZZZX551Channel · crackedINSP OF THE PILOT SEAT SUPPORT STRUCTURE FOUND P/N 5011011-7 GUSSETT, P/N 5015019-1, AND 5015019-3 CHANNELS HAD CRACKED AND FAILED. THERE IS NO ACCESS TO P/N 501101107 FOR INSPECTION AND IT IS BELIEVED THIS PART FAILED FIRST PUTTING HEAVY LOAD ON CHANNELS.SDR 97ZZZX568Doubler · crackedFOUND LOWER INTERNAL DOUBLER (RIB CAP) CRACKED, WS 106.79, 1.5 INCHES LONG STARTING AT AFT SIDE OF GEAR DOOR HINGE CUT OUT. ALSO, ADJACENT LOWER WING SKIN CRACKED SAME LOCATION, SAME CRACK. FOUND ON BOTH WINGS.SDR CA970121001Actuator · failed(CAN) AIRCRAFT WAS MAKING A NORMAL LANDING WITH THREE DOWN AND LOCKED LIGHTS ON. UPON TOUCHDOWN AND AT THE END OF THE ROLL OUT THE NOSE GEAR COLLAPSED WITHOUT WARNING. MAINTENANCE GOT THE AIRCRAFT TO SERVICE AND REMOVED THE NOSE LANDING GEAR ACTUATOR AND SENT SDR 97ZZZX441Distributor Gear · strippedAFTER TAKEOFF, THE RIGHT ENGINE STARTED RUNNING ROUGH. PILOT RECEIVED CLEARANCE TO LAND. AFTER LANDING, PILOT PERFORMED MAG CHECK TAXIING BACK TO GATE. LEFT MAG WAS DEAD. MECHANIC CHANGED MAGNETO, TIMED TO ENGINE, RAN UP GOOD. ON DISASSEMBLY OF MAG, FOUNDSDR 97ZZZX273Cover Assy · leakingOIL PUMP COVER IMPROPERLY INSTALLED BY OVERHAULER CAUSING A SERIOUS LEAK. RE-SEALED COVER PER TCM O/H MANUAL. FIXED THE PROBLEM.SDR 97ZZZX272Spring Seat · missingINSTALLED NEWLY OVERHAULED ENGINE AND DURING PRE-OILING COULD NOT GET OIL PRESSURE. FOUND THAT SPRING SEAT P/N 63153 WAS MISSING FROM OIL PRESSURE RELIEF HOUSING. INSTALLED THE MISSING PART, FIXED THE PROBLEM.SDR 97ZZZX271Plunger · fod malfunctionMECHANIC NOTICED THAT OIL PRESSURE DROPPED TO ZERO WHEN THROTTLE WAS RETARDED. FOUND 3 PIECES OF SAFETY WIRE STUCK UNDER OIL PRESSURE RELIEF VALVE. REMOVED THE WIRE AND OPS CHECKED GOOD.SDR EY2R9601260Retainers · corrodedBLADES, SN'S F44301YS, F44956YS, AND F44460YS, FOUND CORRODED.SDR 96ZZZX6097Pump · failedON TAKEOFF ROLL, THE RIGHT ENGINE QUIT. THE PILOT MADE REJECTED TAKEOFF PROCEDURES. NO DAMAGE TO A/C OR PERSONAL. INVESTIGATION SHOWED THE ENG DRIVEN PUMP FAILED. A TEAR DOWN INSPECTION REVEALED SOME WEAR AND TWO BROKEN BLADES. NO CONCLUSIONS WERE DRAWN ONSDR CA961128023Line · ruptured(CAN) DURING CLIMB ATTITUDE IT WAS NOTICED THAT THE LEFT AND RIGHT HYDRAULIC FLOW LIGHTS CAME ON. INSPECTION OF THE AIRCRAFT FOUND THAT THE RIGHT HAND MAIN ACTUATOR DOWN LINE HAD RUPTURED.SDR BSAA112096Controller · stickingBIL - RIGHT FUEL FLOW LAGGED AND THEN MANIFOLD PRESSURE SPIKED. STICKING WASTEGATE CONTROLLER. WASTEGATE CONTROLLER DISASSEMBLED, CLEANED, INSPECTED, AND REASSEMBLED WITH NEW SEALS. THE OLD SEALS SHOWED SIGNS OF WEAR IN SOME AREAS. GROUND RUN AND LEAK CHECSDR BSAAA111396Fuel Pump · out of adjustBIL - RIGHT ENGINE SURGING. FUEL FLOW WAS GOING OVER RED LINE AND CAUSED THE ENGINE TO FLOOD OUT. ADJUSTED ENGINE DRIVEN FUEL PUMP TO SPECS/GROUND RUN OK. (M)SDR 97ZZZX361Line · leaksFLIGHT CREW NOTICED HYD LEAKAGE INBD WING. INSPECTION NOTED PIN HOLE IN LINE AT HYD FLOW SWITCH AREA. REPLACED LINE AND SERVICED SYSTEM. DETERIORATION OF LINE WAS CAUSE FOR LEAKAGE. SUBMITTER RECOMMENDS PRESSURE TESTS CONTINUE, BUT PREVENTIVE MAINT SHOULD SDR 96ZZZX6001Hub · crackedPROPELLER RECEIVED FOR OVERHAUL. AFTER DISASSEMBLY, DISCOVERED HUB CRACK IN NR 2 BLADE SOCKET, 2 THREADS IN 3 DEGREE TO 5 DEGREE POSITION. ALSO, BLADE RACES AND BALLS CORRODED. (WATER IN THE HUB).SDR EY2R9601196Hub · corrodedCORROSION FOUND ON HUB.SDR EY2R9601195Bearing · corrodedRETAIN BEARING FOUND CORRODED.SDR EY2R9601194Bearing · corrodedRETAIN BEARING FOUND CORRODED.SDR EY2R9600159Hub · crackedPROP HUB ASSY CRACKEDSDR 96ZZZX5658Post Light · shortedPILOT REPORTED SEEING A SMALL AMOUNT OF SMOKE FROM UNDER COPILOT'S INSTRUMENT PANEL AND SMELLING SOMETHING 'ELECTRICAL' BURNING. UPON INSPECTION, A POST LIGHT WAS FOUND SHORTED. NO CIRCUIT BREAKERS TRIPPED. A VERY THIN SPRING INSIDE THE SCREW ON CONNECTOR BSDR 96ZZZX5572Flow Valve · stickingWING DEICE BOOTS DID NOT FULLY DEFLATE AFTER NORMAL CYCLE. LEFT FLOW VALVE STUCK PARTIALLY OPEN. INSTALLED NEW VALVE. OPS CHECKED NORMAL.SDR 96ZZZX5569Control Cable · frayedDURING INSPECTION RIGHT HAND FLAP RETURN CABLE WAS FOUND FRAYED. SEVERAL STRANDS BROKEN AT A PULLEY. REPLACED CABLE, RIGGED PER MM. SUGGEST CLOSE INSPECTION OF CABLES AT PULLEYS.SDR 96ZZZX5557Limit Switch · arms looseFLAPS FOUND HANGING DOWN APROXIMATELY 1 INCH AT INSPECTION. DISCOVERED FLAP GEARBOX LIMIT SWITCH ACTUATING ARM LOOSE ON SHAFT. FLAP PRE-SELECT SWITCH FAILED AND FLAPS DID NOT STOP. REPLACED BENT PUSH/PULL TUBES AND GEARBOX RIGGED AND OPS CHECKED SYSTEM.SDR EY2R9601080Bearing · corrodedBALL BEARING CORRODED.SDR EY2R9601025Blade · corrodedBLADES, SN'S K100294YS, K100298YS, K100724YS, FOUND CORRODED.SDR CA961009008Line · cracked(CAN) ON WALK AROUND PILOT FOUND POOL OF HYDRAULIC FLUID UNDER LEFT WHEEL WELL. FLANGE ON GEAR DOWN LINE FOUND CRACKED.SDR 96ZZZX5239Turbocharger · seal failedDURING PRE-OILING OF NEWLY INSTALLED TCM REBUILT ENGINE, OIL LEAKED OUT OF EXHAUST TAILPIPE. FOUND OIL POURING FROM TURBINE SHAFT LIKE SEAL WAS NOT INSTALLED.
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