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 = '369D' 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 = '369D' 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 AGQA065542Damper · weakMLG DAMPER IS WEAK.SDR AGQA065541Damper · weakMLG DAMPER IS WEAK.SDR AGQA065537Hub · wornTAIL ROTOR HUB IS WORN EXCESSIVELY.SDR AGQA065536Gps · failedGPS UNABLE TO FIND SATELLITES.SDR 20000412SH021Fitting · looseDURING INSPECTION, DISCOVERED THE FIREWALL FUEL FITTING (BULKHEAD FITTING) WAS LOOSE IN THE FIREWALL. RE-TORQUED JAM NUT. (X)SDR 20000412SH020Seal · leakingDURING INSPECTION, FOUND THE TAIL ROTOR OUTPUT SEAL LEAKING. REPLACED SEAL. (X)SDR 2000ZZZX272Strap · crackedMAIN ROTOR HUB STRAP PACK ASSY WAS FOUND WITH ONE CRACKED LEG AT 226.2 HOURS TSO, SECOND CRACK FOUND AT 542.1 HOURS. BOTH CRACKS WERE IN THE LAG (TRAILING EDGE) LEG OF THE SAME PACK. THIRD AND FAILING CRACK WAS FOUND AT 578.8 HOURS TSO. REPLACED WITH ZERO HRSDR CA991229031Sprag Clutch · broken(CAN) DURING 300 HOUR INSPECTION OF THE O/R CLUTCH ASSY, THE SPRAG ASSY (S/N 5433) WAS FOUND TO HAVE A PIECE OF ONE OF THE SPAGS BROKEN OFF. THE PIECE WAS APPRX 1/4 X 1/4 INCH AND CAME FROM THE INSIDE DIAMETER OF THE SPRAG CLUTCH.SDR CA991208092Bearing · wrong part(CAN) AMO RECEIVED SG AND FOUND THE A.D.E. BEARING TO BE NOISY AND ROUGH AND ALSO UNAPPROVED. PROPER OEM BEARINGS INSTALLED P/N 03-6009-23. ARMATURE WAS THEN RESURFACED, BALANCED AND BRUSHES WERE SEATED. UNAPPROVED BEARINGS WERE QUARANTINED.SDR CA991103028Spring · cracked(CAN) SPRING COIL (DAMPER) CRACKED APPROXIMATELY HALF WAY THROUGH WIRE.SDR CA991229051Bolt · loose(CAN) BOLT FOR THE FWD T/R DRIVESHAFT COUPLING WAS FOUND LOOSE. BOLT REPLACED.SDR CA991103019Bracket · failed(CAN) DURING ROUTINE INPSPECTION (UNDER THE FRONT MIDDLE SEAT), THE BEARING CAP WAS FOUND BROKEN ON THE FORWARD SIDE ON THE COLLECTIVE/CYCLIC ASSEMBLY.SDR CA000110004Bearing · making metal(CAN) INPUT ALIGNMENT BEARING MAKING METAL. (CHIP LITE IN CRUISE). GEARBOX STRIPPED TO DETERMINE CAUSE OF FAILURE.SDR 99ZZZX4332Seal · delaminatedDURING REMOVAL OF TURBINE SECTION, A PREVIOUSLY REPAIRED AREA AROUND THE TURBINE SEAL BOSS ON THE GEARBOX COVER HAD DELAMINATED. REPLACED GEARBOX.SDR LS1R99108Indicator · intermittentENGINE OIL TEMPERATURE INDICATOR INTERMITTENTLY JUMPS. REMOVED AND REPLACED. (X)SDR LS1R99107Switch · failedFUEL BYPASS CHECK. DID NOT MAKE CONTACT UNDER PRESSURE. REMOVED AND REPLACED. (X)SDR LS1R99104Indicator · erraticENGINE OIL TEMPERATURE ERRATIC. SOMETIMES HIGH AND SOMETIMES LOW. REMOVED AND REPLACED. (X)SDR 99ZZZX4333Combustion Liner · crackedDURING REPLACEMENT OF TURBINE, THE COMBUSTION LINER WAS FOUND CRACKED AT THE EXPANSION SLOTS AT THE DOUBLE LIP AND THE FUEL NOZZLE FERRULE HAS A DEEP STEP WORN AT THE 6 O'CLOCK POSITION.SDR CA000110002Bearing · making metal(CAN) INPUT ALIGNMENT BEARING MAKING METAL (CHIP LITE IN FLIGHT). GEARBOX STRIPPED TO DETERMINE CAUSE OF METAL GENERATION.SDR CA991027045Bearing · damaged(CAN) PT GOVERNOR LEVER BEARINGS ARE DEVELOPING FLAT SPOTS INTERNALLY AND EXTERNALLY WHICH DIRECTLY AFFECTS GOVERNOR SPRING TENSION WHICH IN TURN THEN CAUSES THE GOVERNOR TO BLEED OFF EARLY. THE NET EFFECT IS DROOP.SDR CA000404011Pin · broken(CAN) M/R BLADE FOLDING PIN FOUND BROKEN DURING REMOVAL FOR 300 HOUR INSPECTION. ALL THE PINS WERE SUBSEQUENTLY REMOVED FOR INSPECTION.SDR CA991007035Governor · failed(CAN) GOVERNOR NOT MAINTAINING ROTOR RPM AND GRADUALLY DEGRADING. UNIT HAD ONLY BEEN INSTALLED FOR 53 HOURS. UNIT REPLACED.SDR CA991027064Blower · failed(CAN) OIL COOLER BLOWER VIBRATING EXCESSIVELY AND ALSO SHOWED SIGNS OF GREASE LOSS.SDR 99ZZZX3858Bleed Valve · inoperativePILOT ENCOUNTERED NUMEROUS RAPID COMPRESSOR STALLS IN A HIGH POWER SITUATION. FOUND SIDE SLOP ON BLEED VALVE POPPET AND A RATCHETY FEEL DURING MANUAL ACTUATION. REPLACED BLEED VALVE.SDR CA991229049Indicator · inaccurate(CAN) TOT GUAGE READS INACCURATELY. UNIT REPLACED.SDR CA991027065Indicator · inaccurate(CAN) 16 PERCENT TACH NEEDLE SPLIT AT THE HIGH END OF THE RANGE.SDR 99ZZZX3975Warning Unit · malfunctionedEPO BOX HAS ENGINE OUT LIGHT AND WARNING HORN ACTIVATED DURING FLIGHT. REMOVED AND REPLACED.SDR 99ZZZX3894Tach Generator · damagedCANNON PLUG BENT AND RIVETS TORN OUT OF HOUSING. REMOVED AND REPLACED.SDR 99ZZZX3893Hour Meter · slowHOUR METER RUNS SLOW. REMOVED AND REPLACED.SDR 99ZZZX3892Interphone · failedNO SIDE TONES. NO INTERCOM. WILL NOT TRANSMIT. REMOVED AND REPLACED.SDR CA991027052Bearing · failed(CAN) SUSPECT FAILURE OF ELASTOMETRIC FORK/HINGE BEARING AS T/R WAS DIFFICULT TO BALANCE.SDR 99ZZZX3546Line · crackedAIR LINE UNDER BRADING ON FLEX PORTION CRACKED. REMOVED AND REPLACED.SDR 99ZZZX3545Link Assy · wornDURING 100-HOUR INSPECTION, FOUND BEARING WORN BEYOND LIMITS. REMOVED AND REPLACED.SDR 99ZZZX3542Indicator · reads highHIGH TOT READING IN A HOVER. OUT OF PARAMETERS WITH TEST UNIT. REMOVED AND REPLACED.SDR 99ZZZX3534Bleed Valve · malfunctionewdENGINE HAD LOW POWER DETERMINED THAT THE BLEED VALVE WAS NOT FULLY CLOSING. REMOVED AND REPLACED.SDR CA990915053Leg · cracked(CAN) GEAR LEG ASSEMBLY TO BRACE ASSEMBLY CRACKED AT BOLT HOLE.SDR 99ZZZX3855Damper Pin · looseDURING POST-FLIGHT, THE 'GREEN' MAIN ROTOR DAMPER PIN WAS FOUND LOOSE. IT HAD WORKED UP TO A POINT WHERE THE BALE WAS CONTACTING THE DAMPER CLEVIS ALTHOUGH IT WAS STILL ENGAGED ON THE PIN.SDR 99ZZZX3285Case Halves · damagedDRESSED OUT MINOR FOD DAMAGE. REMOVED AND REPLACED.SDR 99ZZZX3287Fuel Cell · crackedFUEL CELL HAS SLIGHT HAIRLINE CRACK IN TOP OF BLADDER AROUND PLATE. REMOVED AND REPLACED.SDR CA991027048Line · chafed(CAN) OIL LEAK TRACED TO MGB OIL LINE WHICH WAS CHAFED THROUGH BY A CLAMP.SDR 99ZZZX3286Clock · damagedKNOB BROKEN FROM SHAFT. REMOVED AND REPLACED.SDR 99ZZZX3856Bleed Valve · inoperativeDURING THROTTLE ROLL-ON DURING POWER RECOVERY FROM PRACTICE AUTOROTATION, THE PILOT EXPERIENCED A COMPRESSOR STALL. REPLACED BLEED VALVE.SDR 99ZZZX3859Ignition Lead · damaged(ALLISON EQUIVALENT P/N 6870855) ON INSPECTION, THE CONTACT SLEEVE AT THE 16NOTOR END WS FOUND TO BE MISSING THE CIRCLIP RETAINER AND THE CONTACT SLEEVE HAD SLIPPED BACK INTO THE INSULATOR.SDR 99ZZZX3857Damper Pin · looseDURING 100-HOUR INSPECTION, THE MAIN ROTOR DAMPER PINS WERE FOUND LOOSE AND ONE, THE 'BALE', WAS NOT ENGAGED PROPERLY. (THE PIN HAVING RISEN SO HIGH AS TO FORCE THE BALE OFF OF THE INDEX). INSPECTED, ADJUSTED, AND RE-INSTALLED TWO EACH (RED AND YELLOW).SDR LS1R99102Line · crackedNOTICED BLACK SOOT ON CUSTOMER BLEED LINE TO HEATER. FOUND AIR LEAKING OUT BRAID LINE AREA. REMOVED AND REPLACED. FOUND MATERIAL CRACKS ON FLEX PART OF LINE. (X)SDR CA990728029Window · separated(CAN) RIGHT REAR DOOR WINDOW DEPARTED ROTORCRAFT DURING CRUISE. THIS WINDOW HAD A PREVIOUS CRACK AND WAS A RUBBER MOUNTED WINDOW.SDR 99ZZZX2770Gps · damagedNO LIGHTS OR ANYTHING, SOMETHING LOOSE INSIDE. REMOVED AND REPLACED.SDR 99ZZZX2769Damper · debondedDEBONDED AT OUTBOARD CENTER. REMOVED AND REPLACED.SDR 99ZZZX2607Exhaust Stack · crackedEXHAUST STACK IS CRACKED. REMOVED AND REPLACED.SDR 99ZZZX2602Governor · malfunctionedGOVERNOR SLOW TO RESPOND. REMOVED AND REPLACED.
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