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 = '212' 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 = '212' 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 HEEA079555Line · crackedMAIN ROTOR GEARBOX HAS A CRACKED LINE. REPAIRED LINE.SDR HEEA079390Tarsyn · malfunctionedTARSYN333 MALFUNCTIONS, PILOT`S ATTITUDE SYSTEM CIRCUIT BREAKER POPPING. REPLACED WITH SERVICEABLE UNIT.SDR EHA2002F00004Cargo Hook · inoperativeDURING WORK WITH THE FORREST SERVICE USING BAMBI BUCKETS FOR WATER BOMBER OPERATIONS, THE AIRCRAFT EXPERIENCED AN UNCOMMANDED EXTERNAL LOAD RELEASE. THE AIRCRAFT WAS FLOWN TO THE MAIN BASE WHERE A COMPLETE AND THOROUGH ELECTRICAL EVALUATION AND, AS A PRECAUTISDR EHA2002F00003Thermocouple · failedAFTER SEVERAL FLIGHTS AND SUBSEQUENT CHANGE OF PILOTS, THERE WAS NO T5 INDICATION DURING ENGINE START ON NR 2 ENGINE. DURING VISUAL INSPECTION IT WAS NOTED THAT A STUD HAD BROKEN OFF OF THE THERMAL COUPLE TERMINAL BLOCK TO WHICH EXTERNAL WIRING HARNESS CONNECSDR HEEA079246Indicator · stuckHYDRAULIC PRESSURE TEMPERATURE INDICATOR NEEDLE STICKING ON HIGH SIDE. REPLACED WITH SERVICEABLE PART.SDR EHA2002F00001Control Servo · inoperativeAFTER REPLACING THE TAIL ROTOR SERVO WITH A TESTED, (TIME CONTINUED), SERVICEABLE UNIT, A MAINTENANCE OPERATIONAL CHECK FLIGHT WAS CONDUCTED. DURING THE MOC FLIGHT, THE UPPER SEAL FOR THE SERVO FAILED, CAUSING LOSS OF NR1 HYDRAULIC PRESS. THE AIRCRAFT RETURNSDR CA020621010Bearing · failed(CAN) SUMP CHIP INDICATION DURING GROUND RUN PRIOR TO FLIGHT. METAL CONTAMINATION OF INTERNAL FILTER AND SUMP CHIP PLUG.TRANSMISSION REMOVED FROM SERVICE, TEARDOWN CARRIED OUT. HYDRAULIC QUILL DUPLEX BEARING IDENTIFIED AS SOURCE OF METAL GENERATION.SDR HEEA079090Line · crackedCRACKED LINE. REPLACED WITH SERVICEABLE PART.SDR HEEA079089Transceiver · inoperativeDME/TACAN TRANSCEIVER WILL NOT TRANSMIT OR RECEIVE. REPLACED WITH SERVICEABLE UNIT.SDR EHA2002F0000ACargo Hook · malfunctionedUTILIZING A BAMBI BUCKET FOR WATER BOMBER, AC EXPERIENCED 2 UNCOMMANDED LOAD RELEASES. MAINT SUSPECTED A PROBLEM WITH D-RING COMPATIBILITY WAS CONDUCTED WITH NO ANOMILIES NOTED. ELEC AND MANUAL LOAD JETTISON SYS WERE TESTED, NO ANOMILIES NOTED. SEVERAL LOADSDR EHA2002F00000Wire · defectiveFLOW SWITCH HAD A BROKEN WIRE FROM STOCK. CAUSED AIRCRAFT TO HAVE LATE DEPARTURESDR HEEA078493Gearbox · making metalNR 1 MAIN ROTOR COMBINING GEARBOX IS MAKING METAL.SDR HEEA078487Gearbox · making metalMAIN ROTOR COMBINING GEARBOX MAKING METAL.SDR HEEA078485Gearbox · corrodedGEARBOX HAS CORROSION ON CASE.SDR YTRR078434Diaphragm · rupturedBLEED VALVE LEAKING DUE TO RUPTURED DIAPHRAM.SDR HEEA078542Crosstube · failedDURING PASSENGER LOADING (ENGINES SECURED) AFT CROSSTUBE FAILED ONE INCH OUTBOARD OF RIGHT HAND ATTACHMENT POINT (STRESS MARKS ON TUBE INDICATES FAILURE STARTED AT THE 12 O`CLOCK POSITION). AIRCRAFT SETTLED TO THE RIGHT RESULTING IN DAMAGE TO RIGHT HAND AFT FSDR CA020430011Bearing · failed(CAN) INFLIGHT ILLUMINATION OF TRANSMISSION OIL PRESSURE LIGHT, CONFIRMED BY VISUAL INDICATION OF LOW OIL PRESSURE INDICATION (40PSI). EMERGENCY PROCEDURES INITIATED, PRESSURE INDICATION WENT TO ZERO AFTER A FURTHER 6 MINS OF FLIGHT. EMERGENCY LANDING CARRIED SDR HEEA078538Transceiver · failedTRANSCEIVER FAILED 2 YEAR INSPECTION.SDR HEEA078533Drive Gear · wornWORN DRIVE SPLINES. REPLACED WITH SERVICEABLE FUEL PUMP.SDR CA020409003Actuator · seized(CAN) ROTARY ACTUATOR SEIZED AND HAS NO SCHEDULED MAINTENANCE OR CHECK INTERVAL.SDR CA020408002Seal · leaking(CAN) MANUAL FCU LEAKS AT CONTROL SHAFT SEAL, INTERCONNECT SIDE.SDR YTRR077999Bushing · wornSWASHPLATE SUPPORT BUSHINGS AT GIMBAL RING MOUNT HAD ELONGATED BOLT HOLE. COMPONENT HAD BEEN IN SERVICE FOR APPROXIMATELY HALF OF ITS LIFE.SDR CA020318004Turbine Wheel · damaged(CAN) DURING HELI-SKI OPRATIONS UNUSUAL, INTERMITTENT VIBRATION FELT BY PILOT & NOTICED TO BE INCREASING WITH TIME. ON-SITE ENGINEER BEGAN TROUBLESHOOTING PROCESS BY REMOVING & INSPECTING ENGINE OIL COOLER BLOWER FANS. ON INSTATI ON NR 2 POWER SECTION COULD NOSDR CA020408003Control Box · corroded(CAN) WHILE HOVERING OVER WATER ALL KINDS OF WARNING LIGHTS AND HORNS CAME ON. PARAMETERS LOOKED NORMAL, AIRCRAFT WAS FLOWN TO THE CLOSEST AIRPORT, RPM BOX WAS OPENED AND FOUND CORRODED, WAS SUBSEQUENTLY REPLACED.SDR CA020408001Vent · clogged(CAN) FUEL PRESSURE FLUCTUATED, FUEL PRESSURE TRANSMITTER PORT AND VENT FOUND ALMOST CLOGGED BY MUDDY SUBSTANCE.SDR CA020408004Pump · failed(CAN) IN FLIGHT, FUEL PRESSURE FLUCTUATED AND WENT TO ZERO ON LT FUEL PUMP, CIRCUIT BREAKER POPPED.SDR CA020228012Governor(CAN) COCKPIT INDICATION OF ENGINE TORQUE SPLIT DURING HOVER TAXI, AIRCRAFT RETURNED TO RAMP. TORQUE SPLIT CAUSED BY N2 GOVERNOR FAILURE CONFIRMED BY UNIT REPLACEMENT.SDR LSI2002F00000Filter · failedDURING MAINTENANCE OF THE ENGINE FUEL CONTROL AIR SUPPLY SYSTEM, THE P3 WAS REMOVED FOR INSPECTION AND FOUND TO BE IN TWO PIECES. THE METAL END CAPS ARE NORMALLY WELDED TO METAL SCREEN. THIS PMA FILTER WAS BONDED TOGETHER. THE BOND MATERIAL WAS SO BRITTLE FSDR CA020131003Line · broken(CAN) HE AIRCRAFT NR 1 HYDRAULIC SYSTEM LOST SYSTEM PRESSURE(FLUID LOSS). THE ENGINEER FOUND A HYDRAULIC TUBE BROKEN IN THE MID POINT.SDR CA020131004Chain · broken(CAN) THE HELICOPTER WAS IN CRUISE WHEN ALL OF A SUDDEN THE ROTOR TACH GENERATOR INDICATOR WENT TO ZERO.BACK AT THE BASE AN ENGINEER TROUBLE SHOOTED THE PROBLEM AND FOUND THE TACH. GEN DRIVE WAS DISCONNECTED. THE ROTOR TACH GENERATOR DRIVE IS LOCATED IN THE #1SDR CA020123003Gearbox · contaminated(CAN) IN CRUISE FLIGHT THE PILOT THE PILOT NOTED THE C-BOX CHIP LIGHT FLICKER FAINTLY FOLLOWED SHORTLY BY THE C-BOX OIL PRESSURE CAUTION LIGHT ILLUMINATING.C-BOX OIL PRESSURE WAS OBSERVED DROPPING AND AN UNSCHEDULED BUT NORMAL LANDING PROCEDURE WAS CARRIED OSDR YTRR077529Line · crackedP3 FILTER LINE ON NR 1 ENGINE CRACKED, REPLACED P3 FILTER LINE ASSEMBLY WITH NEW SERVICEABLE ASSEMBLY.SDR CA020104023Oil Jet · mislocated(CAN) DURING INSTALLATION OF MAIN ROTOR MAST ASSEMBLY IT WAS VISUALLY IDENTIFIED THAT THE OIL JET WAS LOCATED IN THE WRONG POSITION FOR CONNECTION OF OIL SUPPLY LINE. PART WAS REPLACED WITH SERVICEABLE UNIT.SDR CA020402004Bearing · failed(CAN) TRANSMISSION REPLACED DUE METAL CONTAMINATION.SDR CA011211002Bolt · bent(CAN) THIS BOLT HOLDS THE TAIL ROTOR DRIVESHAFT COUPLING TO THE INPUT QUILL OF THE 90 DEGREE GEARBOX. WHEN THE BOLT WAS REMOVED FOR SCHEDULED MAINTENANCE (GREASE REPACKING). IT WAD NOTICED THAT IT WAS NOT THE NORMAL COLOR (BLACK) THAN IT WAS NOTICED THAT IT WASDR HEEA077218Fitting · gougedPART IS GOUGED ON TOP AND WAS NOT ACCEPTABLE PER OUR INSPECTORS.SDR CA011116015Bearing · failed(CAN) WHILE IN DESCENT TO THE LANDING AREA THE MAIN ROTOR TRANSMISSION CHIP LIGHT ILLUMINATED. THE PILOT MAINTAINED ITS APPROACH AND LANDED. UPON INSPECTION ON THE CHIP DETECTOR METAL WAS FOUND AND THEN THE WAFFER FILLER WAS CHECKED WHERE MORE METAL WAS FOUND.SDR HEEA076998Indicator · failedSCREEN FLASHES ON THEN OFF WITH DISTORTED IMAGING. REPLACED WITH SERVICEABLE PART.SDR HEEA076997Radar · malfunctionedPILOT HSI CIRCUIT BREAKER POPS IN FLIGHT. REPLACED WITH SERVICEABLE PART.SDR HEEA076985Indicator · failedUNIT READ ZERO. PENDING VENDOR REPAIR.SDR HEEA076981Starter Gen · failedRED GLOW WAS OBSERVED IN THE STARTER GENERATOR FOLLOWED BY SMOKE, STARTER NEVER ENGAGED. REPLACED WITH SERVICEABLE PART.SDR LS1R076935Indicator · inoperativeARTIFICIAL HORIZON WILL NOT COME ON LINE.SDR LS1R076934Indicator · inoperativeARTIFICIAL HORIZON WILL NOT COME ON LINE.SDR LS1R076931Indicator · intermittentINTERMITTENT.SDR GUR2001F00003Pitch Horn · out of toleranceDURING INSPECTION OF THE MAIN ROTOR GRIP PITCH HORN TO GRIP COUNTER BORES, MEASURED THE BORES USING A TELESCOPING GAUGE AND MICROMETERS.SDR GUR2001F00002Pitch Horn · damagedDURING INSPECTION OF THE MAIN ROTOR GRIP PITCH HORN TO GRIP COUNTER BORES USING A TELESCOPING GAUGE AND MICROMETER.SDR GUR2001F00001Pitch Horn · out of toleranceDURING INSPECTION OF THE MAIN ROTOR GRIP PITCH HORN TO GRIP COUNTER BORES, MEASURED THE BORES USING A TELESCOPING GAUGE AND MICROMETER.SDR GUR2001F00000Pitch Horn · out of toleranceDURING INSPECTION OF THE MAIN ROTOR GRIP PITCH HORN TO GRIP COUNTER BORES, MEASURED THE BORES USING A TELESCOPING GAUGE AND MICROMETER.SDR HEEA076269Blade · corrodedCOMPRESSOR BLADE CORRODED.SDR HEEA076261Engine · hot startHOT STARTS. SENT TO PRATT AND WHITNEY FOR INSPECTION AND REPAIR.
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