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 = '60' 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 = '60' 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 2010FA0000080Transmitter · leakingON DECEMBER 29. 2009, ACFT DEPARTED AIRPORT ENROUTE TO GENERAL AIRPORT 18 MILES AWAY WITH APPROX 50 LBS OF FUEL PER SIDE. THE PIC EXPERIENCED AN IN-FLIGHT MALFUNCTION WITH THE RT ENGINE AND HAD TO MAKE AN EMERGENCY LANDING. THE PIC MADE AN UNEVENTFUL SINGLE ENSDR 2009FA0001079O-Ring · crackedACFT EXPERIENCED AN IN-FLIGHT FIRE IN THE LT ENG NACELLE DUE TO A LEAKING LT FUEL FLOW TRANSMITTER. THE TRANSMITTER HAD A BRITTLE/CRACKED O-RING SEAL. THE TRANSMITTER WAS LAST O/H IN 1998. THE RT ENG FUEL FLOW TRANSMITTER HAD BEEN OVERHAULED AT THE SAME TIMSDR CA080208002Elt · failed(CAN) WHEN TESTING THE ELT AT ITS ANNUAL INSP THE ELT HAD NO MODULATION AND NO OUTPUT POWER. THE ELT REPLACED WITH A SERVICEABLE UNIT. (TC NR 20080208002)SDR 0072686Hub · corrodedCORRISION ON PROPELLER HUB.SDR 2001FA0000655Lifter · spalledUPON REMOVAL OF PUSH RODS AND PUSH ROD TUBES FOR RESEAL. THE LIFTERS WERE REMOVED FOR BLEEDING. THE LIFTERS WERE INSPECTED AND WERE FOUND TO HAVE SEVERE SPALLING. MFG WAS NOTIFIED AND ENGINES ARE TO BE REMOVED AND SENT BACK FOR REPAIR. ENGINES HAVE 132.4 HSDR 2001FA0000572Lifter · spalledUPON REMOVAL OF PUSH RODS AND PUSH ROD TUBES FOR RESEAL, THE LIFTERS WERE REMOVED FOR BLEEDING. THE LIFTERS WERE INSPECTED AND WERE FOUND TO HAVE SEVERE SPALLING. MFG WAS NOTIFIED AND ENGINES ARE TO BE REMOVED AND SENT BACK FOR REPAIR. ENGINES HAVE 132.4 HRSSDR 98ZZZX2603Gear · strippedPILOT REPORTED ROUGH RUNNING ENGINE. REMOVED FUEL CONTROL FLOW, CHECKED. FOUND BAD RIGHT MAGNETO. TEETH STRIPPED FROM DISTRIBUTER GEAR.SDR 98ZZZX2574Gear · failedPILOT REPORTED ROUGH RUNNING ENGINE. REMOVED FUEL CONTROL, FLOW CHECKED. FOUND BAD RIGHT MAGNETO. TEETH STRIPPED FROM DISTRIBUTOR GEAR.SDR 98ZZZX1737Washer · missingDURING A 2400 HOUR INSPECTION, THE UPPER RIGHT KEEL BEAM ATTACH BOLT WASHER WAS FOUND MISSING WHICH LET KEEL BEAM BOLT LOOSE. NO OTHER DEFECTS NOTED. INSTALLED NEW WASHER MS20002-6 AND TORQUED TO SPECS.SDR 98ZZZX1736Arm Latch · crackedDURING 2400 HOUR INSPECTION, THE FORWARD AND AFT CABIN DOOR ARM LATCHES WERE FOUND CRACKED DURING EDDY CURRENT REQUIRED INSPECTION. REPLACED ARMS WITH NEW.SDR 98ZZZX1735Bracket · crackedDURING A 2400-HOUR INSPECTION, THE NOSE ROLLER OUTBOARD FORWARD HINGE BRACKET WAS FOUND CRACKED ON LT AND RT FLAPS. REPLACED BRACKET WITH NEW.SDR 98ZZZX1734Bracket · crackedDURING A 2400-HOUR INSPECTION, THE NOSE ROLLER OUTBOARD FORWARD HINGE BRACKET WAS FOUND CRACKED ON LT AND RT FLAPS. REPLACED BRACKET WITH NEW.SDR 98ZZZX1733Bolt · missingDURING A 2400 HOUR INSPECTION, 2 EACH BOLTS WERE FOUND MISSING IN LOWER ATTACH POINT OF VERTICAL STABILZIER. NO OTHER DEFECTS FOUND. INSTALLED NEW BOLTS AN960-416, WASHERS, AND NUTS.SDR 98ZZZX1384Piston Rod · failedAFTER REPLACING WHEEL BRAKE ASSEMBLIES, WENT TO BLEED BRAKE SYSTEM. NO BRAKE RESPONSE ON PILOT'S LEFT BRAKE. TROUBLESHOT TO POWER BRAKE VALVE. FOUND PISTON ROD BROKEN AND LODGED IN OPERATING LINKAGE. THE PILOT HAD NOT REPORTED A PROBLEM WITH THE BRAKE SYSTSDR 97ZZZX3388Fuel Cell · deterioratedFUEL CELL BEGAN LEAKING IN MARCH, 1994; WAS REMOVED AND SENT TO A/C FUEL CELLS WORLDWIDE, INC., FOR REPAIR. A/C CONDEMNED CELL AND REBUILT CELL WAS PURCHASED FOR REPLACEMENT (WORK ORDER NR 9681, INSPECTED 4-12-94) IN APRIL, 1994. OCTOBER, 1996, REPLACEMENT CSDR 97ZZZX3387Fuel Cell · deterioratedFUEL CELL BEGAN LEAKING IN MARCH, 1994; WAS REMOVED AND SENT TO A/C FUEL CELLS WORLDWIDE, INC., FOR REPAIR. A/C CONDEMNED CELL AND REBUILT CELL WAS PURCHASED FOR REPLACEMENT (WORK ORDER NR 9938, INSPECTED 4-18-94) IN APRIL, 1994. JUNE, 1997, REPLACEMENT CELLSDR AU970408Adapter · cracked(AUS) LANDING GEAR ATTACHMENT BRACKET CRACKEDSDR 97ZZZX1888Wire · meltedUNABLE TO REMOVE POWER FROM NR 1 RT DC BUS. FOUND BUTT SPLICES (NYLON) AT P10 ON FRAME 26A WIRE NR P26A10T, P31B10T, P175A10, MELTED TOGETHER. WIRE P175A10 COMES FROM THE AIRSTART LIMITER IN THE GENERATOR CONTROL PANEL. THE AIRSTART LIMITER GETS ITS POWER FSDR 96ZZZX5969Warn Light · stays armedTHE DE-ICE ALCOHOL LOW LEVEL WARNING LIGHT ILLUMINATES ON THE MASTER WARNING PANEL AT AIRCRAFT ROTATION DURING TAKEOFF. ONCE ACTIVATED, THE LIGHT STAYS ILLUMINATED UNTIL POWER IS REMOVED FROM THE AIRCRAFT. LEARJET ISSUED OPTIONAL SERVICE BULLETIN 60-30-1 TO SDR 96ZZZX5741Silencer · rupturedWHILE PERFORMING FINAL ENGINE RUNS AND AIRFRAME SYSTEMS CHECK OUT FOLLOWING INITIAL 300/600 HOUR INSPECTIONS, BOTH ENGINE BLEED AIR SOURCES WERE TURNED ON TO CHECK AIR DISTRIBUTION SYSTEM. CABIN AND COCKPIT WERE SHOWERED WITH FIBERGLASS FROM AIR DUCTS. FOUNDSDR EY2R9601592Blade · damagedBLADE SN D2825, NICKEDSDR EY2R9600837Feathering Sprng · corrodedCORROSION FOUND ON FEATHERING SPRING.SDR 96ZZZX2232Control Unit · failedLEFT STARTER WOULD NOT ROTATE WHEN START WAS SELECTED. REPLACED GENERATOR CONTROL UNIT. SYSTEM WAS RESTORED TO NORMAL.SDR 95ZZZX6178Wye Assy · crackedAN INTENSE IN-FLIGHT FIRE OCCURRED WHEN A CRACK IN THE LEFT ENGINE WYE EXHAUST ASSY DEVELOPED AND ALLOWED HOT EXHAUST GAS TO LEAK THROUGH LOOSE COUPLING INTO ACCESSORY SECTION. THE CRACK IN THE WYE ASSY COULD NOT BE DETECTED UNTIL AIR PRESSURE WAS FORCED INTOSDR 95ZZZX5241Electrical Sys · faultyAIRCRAFT EXPERIENCED ELECTRICAL FAILURE IN-FLIGHT. BOTH GENERATORS DROPPED OFF LINE. SWITCHED TO EMERGENCY BUS AND LANDED WITHOUT FURTHER PROBLEMS. TROUBLESHOT SYSTEM AND WAS UNABLE TO DETERMINE EXACT PROBLEM. INSTALLED NEW GENERATORS SAME PN 6058003-1 LEFSDR 95ZZZX5251Tube · failedHYDRAULIC TUBE LOCATED BETWEEN HYD RESERVOIR AND EXTERNAL SERVICE RETURN FITTING RUPTURED IN-FLIGHT. ACFT LANDED WITHOUT DAMAGE EXCEPT FOR A BLOWN NR 4 TIRE WHEN EMERG BRAKING APPLIED. SUBMITTER SUSPECTS THIS LINE WAS WEAKENED BY REPEATED THERMAL EXPANSION OSDR 95ZZZX5888Skin · corrodedWHEN AIRCRAFT WAS STRIPPED FOR PAINTING, SEVERE CORROSION WAS NOTED WITH HOLES THROUGH SKIN AND INTO HONEYCOMB, APPEARS TO BE INTERGRANULAR CORROSION, POSSIBLY STARTED AT MANUFACTURING PROCESS.SDR 95ZZZX5886Skin · corrodedWHEN AIRCRAFT WAS STRIPPED FOR PAINTING, SEVERE CORROSION WAS NOTED WITH HOLES THROUGH SKIN AND INTO HONEYCOMB. APPEARS TO BE INTERGRANULAR CORROSION, POSSIBLY STARTED AT MANUFACTURING PROCESS.
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