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 = '206B' 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 = '206B' 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 99ZZZX404Frame · corrodedSHOP INSPECTION FOR REPAIR OF LEAKING SHAFT SEALS. FOUND RUST COATING ON FILTER FRAME.SDR 99ZZZX231Indicator · malfunctionedBIG NEEDLE AND LITTLE NEEDLE DO NOT CORRESPOND ON COCKPIT INDICATOR.SDR 98ZZZX4737Indicator · failedROTOR NEEDLE DROPS TO ZERO DURING FLIGHT. REMOVED AND REPLACED.SDR CA981230007Support · cracked(CAN) PILOT REPORTED NOT BEING ABLE TO ADJUST CYCLIC FRICTION. THE FRICTION ADJUSTMENT WOULD TURN, BUT FRICTION WOULD NOT INCREASE. ATTEMPTS AT ADJUSTING THE MINIMUM FRICTION DID NOT WORK. WHEN REMOVING SUPPORT ASSY TO CHANGE THE FRICTION BEARING, A CRACK ISDR 98ZZZX4738Valve · failedVALVE DOES NOT CLOSE COMPLETELY. REMOVED AND REPLACED.SDR 98ZZZX4735Link · wornBEARING WORN. REMOVED AND REPLACED.SDR CA981230031Governor · malfunctioned(CAN) AT 100 PERCENT, THE RPM SURGED UP AND DOWN. THE GOVERNOR WAS REPLACED.SDR 99ZZZX234Line · blockedFAILURE OF PITOT STATIC SYSTEM. BLOCKAGE OF RESTRICTOR FITTING. COMPLETE FAILURE OF STATIC SYSTEM AND LOSS OF MODE C ALT REPORTING.SDR 98ZZZX4734Gauge · stickingERRATIC GAUGE STICKS, DOES NOT GIVE ACCURATE POWER CHECK. REMOVED AND REPLACED.SDR 98ZZZX4204Drive Collar · failed'BELL HELICOPTER TEXTRON HAS ISSUED OPERATION SAFETY NOTICE OSN 206-98-34 AND 206L-98-40 DATED 11-2-98.' BELL HELICOPTER HAS LEARNED OF A RECENT HARD-FOULING CONDITION IN THE FLIGHT CONTROL SYSTEM OF A 206L HELICOPTER THAT RESULTED IN A BROKEN SWASHPLATE DRIVSDR AU981417Tube · misinstalled(AUS) TAIL ROTOR PITCH CONTROL TUBE FITTED TO THE AIRCRAFT WAS A DIFFERENT PART NUMBER TO THE ONE IN THE MAINTENANCE DOCUMENTATION. PART TC: 13,461.SDR CA981125052Case · cracked(CAN) OUTER CASE OF TACHOMETER/GENERATOR FOUND CRACKED.SDR 98ZZZX4353Sensor · mismanufacturedRECEIVED PART FROM BELL HELICOPTER IN REPAIRED CONDITION WITH A FORM 8130 ISSUED BY BF GOODRICH. PART WAS INSTALLED IN AIRCRAFT FOR 23.7 HOURS BEFORE FAILURE. FOUND FLOAT ARM PIVOT PIN MISSING UPON REMOVAL. SUBMITTER SUSPECTS PIN WAS IMPROPERLY STAKED. PINSDR 98ZZZX4082Fitting · crackedUPPER LEFT TAIL BOOM ATTACHMENT FITTING CRACKED. FITTING CRACKED AT THE LEFT LEG THROUGH AFT MOST TWO RIVET HOLES.SDR HAISUPR0009Rib · crackedRIGHT TAILBOOM ATTACH FITTING P/N 206-020-121-010 CRACKED. (PART OF LISTED ASSY.) REPLACED RIB ASSEMBLY.SDR CA981027007Shaft · wrong part(CAN) ON DISASSEMBLY AT OVERHAUL FACILITY, THE APC STARTER/GENERATOR WAS FOUND TO CONTAIN A LUCAS SHAFT AND A LUCAS DAMPENER IN PLACE OF THE APC SHAFT, P/N 150SG1103-2. THE ASSEMBLY ALSO HAD A SECOND DAMPENER DEVICE AT THE ANTI-DRIVE END. SUBMITTER STATED NSDR 98ZZZX4346Fuel Control · malfunctionedFUEL CONTROL SUSPECTED TO ALLOW AIR INTO FUEL SYSTEM.SDR CA981125051Fcu · faulty(CAN) THE FUEL CONTROL WAS INSTALLED FOR 54.3 HOURS AND WAS ADJUSTED SEVERAL TIMES DUE TO POOR STARTING. THE UNIT WOULD WORK WELL FOR A FEW STARTS AND THEN REQUIRE RE-ADJUSTMENT. THE FUEL CONTROL UNIT WAS REPLACED.SDR CA981125050Indicator · reads low(CAN) TOT GAUGE READING 12 TO 14 DEGREES LOW. GAUGE REPLACED.SDR CA981125049Nozzle · faulty(CAN) DURING INSPECTION, THE COMBUSTION LINER WAS FOUND TO HAVE HOT SPOTS. IT IS SUSPECTED THAT POOR SPRAY PATTERN OF THE FUEL NOZZLE CAUSED THIS PROBLEM. THE SUBMITTER STATES THAT THE FUEL NOZZLE WAS ON A TBO EXTENSION.SDR CA981125045Fcu · faulty(CAN) LIGHT OFF ADJUSTMENT WOULD NOT STAY WITHIN LIMITS DURING INSTALLATION. THE FUEL CONTROL WAS REPLACED.SDR CA981125044Servo · failed(CAN) AFTER SERVO INSTALLATION, THE TEST FLIGHT REVEALED CONTROL FEEDBACK. SERVO REPLACED.SDR CA981019013Switch · leaking(CAN) PRESSURE SWITCH LEAKING BETWEEN CONNECTING BOLT AND OUTER CASING. WHEN WORKING ON THE SWITCH, LIGHT CAME 'ON' AND STAYED 'ON'.SDR CA981125042Bulb · failed(CAN) LANDING LIGHT NOT OPERATING ACCORDING TO PILOT. BROKEN WIRE FOUND AT BULB. ALSO, SOME WIRES FOUND BROKEN AT THE GOVERNOR RPM SWITCH.SDR 98ZZZX3653Bearing · failedPARTIAL POWER LOSS, TOT, RISE, AND ENGINE NOISE DURING FLIGHT (LEVEL). ENGINE TEAR-DOWN REVEALED COMPRESSOR BLADES RUBBING CASE HALVES. COMPRESSOR TEAR-DOWN REVEALED NR 1 BEARING FAILURE OF BALL CAGE. SUBMITTER STATED CAUSE UNKNOWN.SDR 98ZZZX4739Governor · failedWHILE PERFORMING FIRE FIGHTING FOR DNR, PILOT FILLED BUCKET AND STARTED CLIMB, ENGINE LOST POWER. PILOT DUMPED WATER WHICH BROUGHT ROTOR POWER-UP. PILOT WAS ABLE TO GET HELICOPTER TO SHORE. HELICOPTER AUTOROTATED AND STRUCK METAL TREE STAKE DAMAGING TAIL ROSDR AU981141Mount · cracked(AUS) TAIL ROTOR GEARBOX MOUNT FORGING CRACKED IN AREA OF THE LEFT REAR STUD HOLE. PART TC: 10,168.SDR CA981125043Swashplate · out of adjust(CAN) PILOT NOTED THAT HYDRAULIC OFF OPERATION WAS STIFF. SWASHPLATE FRICTION REQUIRED ADJUSTMENT. NO DAMAGE FOUND.SDR 98ZZZX3654Actuator · damagedELECTRICAL STUD BROKEN. SENT OUT FOR REPAIR.SDR 98ZZZX3646Housing · damagedOIL FITTING HAS STRIPPED THREADS IN HOUSING. REMOVED AND REPLACED.SDR CA981125036Relay · failed(CAN) STARTER REMAINED ENGAGED WHEN ENGINE SHUT DOWN. HAD TO TURN BATTERY SWITCH OFF TO GET STARTER TO STOP.SDR CA981125046Shaft · scored(CAN) DURING INSPECTION OF TAILROTOR DRIVE, THE SHORT SHAFT UNDER THE OIL COOLER WAS FOUND SCORED.SDR CA981125038Motor · failed(CAN) DEFOG MOTOR FAILED ON TAKEOFF.SDR CA981125040Bearing · overheated(CAN) DUPLEX BEARING RUNNING HOT, SPUES VERY BLACK GREASE.SDR 99ZZZX3041Bearing · failedOUTER RACE OF DUPLEX BEARING BREAKING DOWN.SDR CA981125037Valve · leaking(CAN) ENGINE FAILING THE POWER CHECKS. THE BLEED VALVE DIAPHRAGM WAS LEAKING.SDR CA980916039Tube · melted(CAN) AIRSPEED INDICATOR READING 30-40 KNOTS LOW IN CRUISE. TUBING FROM PITOT HEAD TO 'T' FITTING HAD A HOLE MELTED THROUGH FROM PROXIMITY TO LANDING LIGHT.SDR CA981125033Fcu · faulty(CAN) ENGINE REMAINS AT IDLE WHEN THROTTLE IS ADVANCED TO FULL POWER.SDR 98ZZZX2790Pitch Link · crackedCRACKS AT END OF TUBE WHERE ADJUSTMENT INSERT LOCATED (206-010-356-001). AIRCRAFT TOTAL TIME 9,500 HOURS. FOUND DURING 100-HOUR INSPECTION..SDR 98ZZZX2955Engine · making metalENGINE CHIP LIGHT CAUTION LIGHT ILLUMINATED. PILOT MADE PRECAUTIONARY LANDING AT A FIELD SITE 3 MILES SOUTH OF AIRPORT. CHIP DETECTORS REMOVED AND INSPECTED IAW ALLISON OPERATION AND OVERHAUL MANUAL 10WZ PAG G-1. SMALL CHIPS AND FLAKES WERE NOTED (3), PLUGSSDR 98ZZZX3160Control Cable · brokenON LAST FLIGHT OF THE DAY, ROLLED THE GAS PRODUCER N1 CONTROL TO FLIGHT IDLE. UNABLE TO SHUT ENGINE OFF WITH THROTTLE CONTROL. ENGINE HAD TO BE SHUT DOWN MANUALLY. UPON INVESTIGATION, FOUND CABLE ASSY BROKEN UNDER PILOT'S SEAT DECK. FAILED PART, POSSIBLY BSDR 98ZZZX3409Bulkhead · crackedBULKHEAD WAS CRACKED AT THE LT UPPER CORNER AT THE T/R GEARBOX ATTACHMENT POINT THROUGH THE UPPER ADJACENT RIVET HOLE AND BACK THROUGH THE BULKHEAD RADIUS RE-CONNECTING WITH ANOTHER CRACK PROGRESSING FROM THE ATTACHMENT POINT HOLE FORWARD TOWARD THE TOP RADIUSSDR CA980818021Servo · failed(CAN) NEWLY INSTALLED HYDRAULIC SERVO CAUSING FEEDBACK IN CONTROLS. SERVO REPLACED AND FEEDBACK NIL.SDR CA980804010Bearing · wrong part(CAN) STARTER/GENERATOR IN SHOP FOR OVERHAUL DUE TO 'WORN BEARINGS' ON DISASSEMBLY, UNAPPROVED BEARINGS FOR THIS UNIT WERE FOUND WORN AND DRY.SDR CA981125030Transmission · making metal(CAN) MAIN ROTOR TRANSMISSION MAKING METAL (FLAKES). THE TRANSMISSION INCREASED 25C. SLIGHT OIL PRESSURE DECREASE.SDR CA981125029Bumper · cut(CAN) TAIL ROTOR BUMPER CUT THROUGH AT THE TAIL ROTOR FLAP STOP CONTACT AREA.SDR CA980916037Blade · damaged(CAN) TAIL ROTOR BLADE STATIC STOP BUMPER CUT THROUGH. THIS BLACK COLORED BUMPER IS MUCH THINNER THAN THE ORIGINAL ORANGE/BROWN BELL MANUFACTURED BUMPER.SDR 98ZZZX3555Battery · dischargedBATTERY WILL NOT CRANK AIRCRAFT PAST 12 PERCENT N1. REMOVED AND REPLACED.SDR 98ZZZX3554Battery · overheatedBATTERY OVERHEATED. VOTLAGE REGULATOR WAS OUT OF ADJUSTMENT. ADJUSTED VOLTAGE REGULATOR AND REPLACED BATTERY.SDR 98ZZZX3510Coupling · wornCOUPLING GEARS WORN BEYOND LIMITS. REMOVED AND REPLACED. NORMAL RUN-OUT.
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